A3XX: Seperate Aerodynamics, Improve Drag, Fix EGT Bug
This commit is contained in:
Joshua Davidson
parent
66bafb9480
commit
68505d69d1
11 changed files with 1216 additions and 2311 deletions
399
A319-100-CFM.xml
399
A319-100-CFM.xml
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@ -581,389 +581,20 @@ YAW MOI_________3950000______23089847_______24848934
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<flight_control name="none"/>
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<aerodynamics>
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<aerodynamics file="Systems/a319-aerodynamics.xml" />
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<axis name="LIFT">
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<function name="aero/force/Lift_alpha">
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<description>Lift due to alpha</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<table>
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<independentVar lookup="row">aero/alpha-rad</independentVar>
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<tableData>
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-0.20 -0.900
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0.00 0.103
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0.15 1.600
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0.23 1.900
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0.60 1.000
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</tableData>
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</table>
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</product>
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</function>
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<function name="aero/force/Lift_flap">
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<description>Delta Lift due to flaps</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<table>
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<independentVar lookup="row">fcs/flap-pos-norm</independentVar>
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<tableData>
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0.000 0.00000
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0.290 0.00250
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0.596 0.00700
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0.645 0.01300
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1.000 0.01700
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</tableData>
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</table>
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</product>
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</function>
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<function name="aero/force/Lift_slats">
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<description>Delta Lift due to slats</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>fcs/slat-pos-deg</property>
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<value> 0.01000 </value>
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</product>
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</function>
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<function name="aero/force/Lift_speedbrake">
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<description>Delta Lift due to speedbrake</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>fcs/speedbrake-pos-norm</property>
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<value>-0.15</value>
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</product>
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</function>
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<function name="aero/force/Lift_elevator">
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<description>Lift due to Elevator Deflection</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>fcs/elevator-pos-rad</property>
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<value>0.04</value>
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</product>
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</function>
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</axis>
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<axis name="DRAG">
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<function name="aero/force/Drag_basic">
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<description>Drag at zero lift</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<table>
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<independentVar lookup="row">aero/alpha-rad</independentVar>
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<tableData>
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-1.57 1.260
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-0.26 0.018
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0.00 0.008
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0.26 0.017
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1.57 1.320
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</tableData>
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</table>
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</product>
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</function>
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<function name="aero/force/Drag_induced">
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<description>Induced drag</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>aero/cl-squared</property>
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<value>0.035</value>
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</product>
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</function>
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<function name="aero/force/Drag_mach">
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<description>Drag due to mach</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<table>
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<independentVar lookup="row">velocities/mach</independentVar>
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<tableData>
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0.00 0.000
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0.79 0.000
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1.10 0.023
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1.80 0.015
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</tableData>
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</table>
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</product>
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</function>
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<function name="aero/force/Drag_flap">
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<description>Drag due to flaps</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>fcs/flap-pos-deg</property>
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<value> 0.00090 </value>
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</product>
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</function>
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<function name="aero/force/Drag_slats">
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<description>Drag due to slats</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>fcs/flap-pos-deg</property>
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<value> 0.00120 </value>
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</product>
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</function>
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<function name="aero/force/Drag_gear">
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<description>Drag due to gear</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>gear/gear-pos-norm</property>
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<value>0.025</value>
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</product>
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</function>
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<function name="aero/force/Drag_speedbrake">
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<description>Drag due to speedbrakes</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>fcs/speedbrake-pos-norm</property>
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<value>0.035</value>
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</product>
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</function>
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<function name="aero/force/Drag_beta">
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<description>Drag due to sideslip</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<table>
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<independentVar lookup="row">aero/beta-rad</independentVar>
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<tableData>
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-1.57 1.230
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-0.26 0.050
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0.00 0.000
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0.26 0.050
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1.57 1.230
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</tableData>
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</table>
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</product>
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</function>
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<function name="aero/force/Drag_elevator">
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<description>Drag due to Elevator Deflection</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<abs><property>fcs/elevator-pos-norm</property></abs>
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<value>0.035</value>
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</product>
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</function>
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</axis>
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<axis name="SIDE">
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<function name="aero/force/Side_beta">
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<description>Side force due to beta</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>aero/beta-rad</property>
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<value>-1</value>
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</product>
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</function>
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</axis>
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<axis name="ROLL">
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<function name="aero/moment/Roll_beta">
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<description>Roll moment due to beta</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>metrics/bw-ft</property>
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<property>aero/beta-rad</property>
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<value>-0.1</value>
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</product>
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</function>
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<function name="aero/moment/Roll_damp">
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<description>Roll moment due to roll rate</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>metrics/bw-ft</property>
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<property>aero/bi2vel</property>
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<property>velocities/p-aero-rad_sec</property>
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<value>-0.95</value>
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</product>
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</function>
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<function name="aero/moment/Roll_yaw">
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<description>Roll moment due to yaw rate</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>metrics/bw-ft</property>
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<property>aero/bi2vel</property>
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<property>velocities/r-aero-rad_sec</property>
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<value>0.005</value>
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</product>
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</function>
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<function name="aero/moment/Roll_aileron">
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<description>Roll moment due to aileron</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>metrics/bw-ft</property>
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<property>fcs/left-aileron-pos-rad</property>
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<value>0.20</value>
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</product>
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</function>
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<function name="aero/moment/Roll_rudder">
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<description>Roll moment due to rudder</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>metrics/bw-ft</property>
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<property>fcs/rudder-pos-rad</property>
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<value>0.003</value>
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</product>
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</function>
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</axis>
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<axis name="PITCH">
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<function name="aero/moment/Pitch_alpha">
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<description>Pitch moment due to alpha</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>metrics/cbarw-ft</property>
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<property>aero/alpha-rad</property>
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<value>-0.6</value>
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</product>
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</function>
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<function name="aero/moment/Pitch_elevator">
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<description>Pitch moment due to elevator</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>metrics/cbarw-ft</property>
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<property>fcs/elevator-pos-rad</property>
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<table>
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<independentVar lookup="row">velocities/mach</independentVar>
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<tableData>
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0.0 -1.900
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2.0 -0.900
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</tableData>
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</table>
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</product>
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</function>
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<function name="aero/moment/Pitch_damp">
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<description>Pitch moment due to pitch rate</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>metrics/cbarw-ft</property>
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<property>aero/ci2vel</property>
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<property>velocities/q-aero-rad_sec</property>
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<value>-140</value>
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</product>
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</function>
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<function name="aero/moment/Pitch_alphadot">
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<description>Pitch moment due to alpha rate</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>metrics/cbarw-ft</property>
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<property>aero/ci2vel</property>
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<property>aero/alphadot-rad_sec</property>
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<value>-1</value>
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</product>
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</function>
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</axis>
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<axis name="YAW">
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<function name="aero/moment/Yaw_beta">
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<description>Yaw moment due to beta</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>metrics/bw-ft</property>
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<property>aero/beta-rad</property>
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<value>0.12</value>
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</product>
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</function>
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<function name="aero/moment/Yaw_damp">
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<description>Yaw moment due to yaw rate</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>metrics/bw-ft</property>
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<property>aero/bi2vel</property>
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<property>velocities/r-aero-rad_sec</property>
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<value>-0.2</value>
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</product>
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</function>
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<function name="aero/moment/Yaw_rudder">
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<description>Yaw moment due to rudder</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>metrics/bw-ft</property>
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<property>fcs/rudder-pos-rad</property>
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<value>-0.2</value>
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</product>
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</function>
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<function name="aero/moment/Yaw_aileron">
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<description>Adverse yaw</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>metrics/bw-ft</property>
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<property>fcs/left-aileron-pos-rad</property>
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<value>0</value>
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</product>
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</function>
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</axis>
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</aerodynamics>
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<external_reactions>
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<force name="pushback" frame="BODY">
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<location unit="IN">
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<x>294</x>
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<y>0</y>
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<z>-149</z>
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</location>
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<direction>
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<x>1</x>
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<y>0</y>
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<z>0</z>
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</direction>
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</force>
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</external_reactions>
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<external_reactions>
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<force name="pushback" frame="BODY">
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<location unit="IN">
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<x>294</x>
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<y>0</y>
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<z>-149</z>
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</location>
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<direction>
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<x>1</x>
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<y>0</y>
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<z>0</z>
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</direction>
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</force>
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</external_reactions>
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</fdm_config>
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399
A319-100-IAE.xml
399
A319-100-IAE.xml
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@ -581,389 +581,20 @@ YAW MOI_________3950000______23089847_______24848934
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<flight_control name="none"/>
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<aerodynamics>
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<aerodynamics file="Systems/a319-aerodynamics.xml" />
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<axis name="LIFT">
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<function name="aero/force/Lift_alpha">
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<description>Lift due to alpha</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<table>
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<independentVar lookup="row">aero/alpha-rad</independentVar>
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<tableData>
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-0.20 -0.900
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0.00 0.103
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0.15 1.600
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0.23 1.900
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0.60 1.000
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</tableData>
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</table>
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</product>
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</function>
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<function name="aero/force/Lift_flap">
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<description>Delta Lift due to flaps</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<table>
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<independentVar lookup="row">fcs/flap-pos-norm</independentVar>
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<tableData>
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0.000 0.00000
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0.290 0.00250
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0.596 0.00700
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0.645 0.01300
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1.000 0.01700
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</tableData>
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</table>
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</product>
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</function>
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<function name="aero/force/Lift_slats">
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<description>Delta Lift due to slats</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>fcs/slat-pos-deg</property>
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<value> 0.01000 </value>
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</product>
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</function>
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<function name="aero/force/Lift_speedbrake">
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<description>Delta Lift due to speedbrake</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>fcs/speedbrake-pos-norm</property>
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<value>-0.15</value>
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</product>
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</function>
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<function name="aero/force/Lift_elevator">
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<description>Lift due to Elevator Deflection</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>fcs/elevator-pos-rad</property>
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<value>0.04</value>
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</product>
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</function>
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</axis>
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<axis name="DRAG">
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<function name="aero/force/Drag_basic">
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<description>Drag at zero lift</description>
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<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">aero/alpha-rad</independentVar>
|
||||
<tableData>
|
||||
-1.57 1.260
|
||||
-0.26 0.018
|
||||
0.00 0.008
|
||||
0.26 0.017
|
||||
1.57 1.320
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_induced">
|
||||
<description>Induced drag</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>aero/cl-squared</property>
|
||||
<value>0.035</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_mach">
|
||||
<description>Drag due to mach</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<tableData>
|
||||
0.00 0.000
|
||||
0.79 0.000
|
||||
1.10 0.023
|
||||
1.80 0.015
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_flap">
|
||||
<description>Drag due to flaps</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/flap-pos-deg</property>
|
||||
<value> 0.00090 </value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_slats">
|
||||
<description>Drag due to slats</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/flap-pos-deg</property>
|
||||
<value> 0.00120 </value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_gear">
|
||||
<description>Drag due to gear</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>gear/gear-pos-norm</property>
|
||||
<value>0.025</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_speedbrake">
|
||||
<description>Drag due to speedbrakes</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/speedbrake-pos-norm</property>
|
||||
<value>0.035</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_beta">
|
||||
<description>Drag due to sideslip</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">aero/beta-rad</independentVar>
|
||||
<tableData>
|
||||
-1.57 1.230
|
||||
-0.26 0.050
|
||||
0.00 0.000
|
||||
0.26 0.050
|
||||
1.57 1.230
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_elevator">
|
||||
<description>Drag due to Elevator Deflection</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<abs><property>fcs/elevator-pos-norm</property></abs>
|
||||
<value>0.035</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="SIDE">
|
||||
|
||||
<function name="aero/force/Side_beta">
|
||||
<description>Side force due to beta</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>aero/beta-rad</property>
|
||||
<value>-1</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="ROLL">
|
||||
|
||||
<function name="aero/moment/Roll_beta">
|
||||
<description>Roll moment due to beta</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/beta-rad</property>
|
||||
<value>-0.1</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Roll_damp">
|
||||
<description>Roll moment due to roll rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/bi2vel</property>
|
||||
<property>velocities/p-aero-rad_sec</property>
|
||||
<value>-0.95</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Roll_yaw">
|
||||
<description>Roll moment due to yaw rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/bi2vel</property>
|
||||
<property>velocities/r-aero-rad_sec</property>
|
||||
<value>0.005</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Roll_aileron">
|
||||
<description>Roll moment due to aileron</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>fcs/left-aileron-pos-rad</property>
|
||||
<value>0.20</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Roll_rudder">
|
||||
<description>Roll moment due to rudder</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>fcs/rudder-pos-rad</property>
|
||||
<value>0.003</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="PITCH">
|
||||
|
||||
<function name="aero/moment/Pitch_alpha">
|
||||
<description>Pitch moment due to alpha</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/cbarw-ft</property>
|
||||
<property>aero/alpha-rad</property>
|
||||
<value>-0.6</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Pitch_elevator">
|
||||
<description>Pitch moment due to elevator</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/cbarw-ft</property>
|
||||
<property>fcs/elevator-pos-rad</property>
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<tableData>
|
||||
0.0 -1.900
|
||||
2.0 -0.900
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Pitch_damp">
|
||||
<description>Pitch moment due to pitch rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/cbarw-ft</property>
|
||||
<property>aero/ci2vel</property>
|
||||
<property>velocities/q-aero-rad_sec</property>
|
||||
<value>-140</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Pitch_alphadot">
|
||||
<description>Pitch moment due to alpha rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/cbarw-ft</property>
|
||||
<property>aero/ci2vel</property>
|
||||
<property>aero/alphadot-rad_sec</property>
|
||||
<value>-1</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="YAW">
|
||||
|
||||
<function name="aero/moment/Yaw_beta">
|
||||
<description>Yaw moment due to beta</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/beta-rad</property>
|
||||
<value>0.12</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Yaw_damp">
|
||||
<description>Yaw moment due to yaw rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/bi2vel</property>
|
||||
<property>velocities/r-aero-rad_sec</property>
|
||||
<value>-0.2</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Yaw_rudder">
|
||||
<description>Yaw moment due to rudder</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>fcs/rudder-pos-rad</property>
|
||||
<value>-0.2</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Yaw_aileron">
|
||||
<description>Adverse yaw</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>fcs/left-aileron-pos-rad</property>
|
||||
<value>0</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
</aerodynamics>
|
||||
|
||||
<external_reactions>
|
||||
<force name="pushback" frame="BODY">
|
||||
<location unit="IN">
|
||||
<x>294</x>
|
||||
<y>0</y>
|
||||
<z>-149</z>
|
||||
</location>
|
||||
<direction>
|
||||
<x>1</x>
|
||||
<y>0</y>
|
||||
<z>0</z>
|
||||
</direction>
|
||||
</force>
|
||||
</external_reactions>
|
||||
<external_reactions>
|
||||
<force name="pushback" frame="BODY">
|
||||
<location unit="IN">
|
||||
<x>294</x>
|
||||
<y>0</y>
|
||||
<z>-149</z>
|
||||
</location>
|
||||
<direction>
|
||||
<x>1</x>
|
||||
<y>0</y>
|
||||
<z>0</z>
|
||||
</direction>
|
||||
</force>
|
||||
</external_reactions>
|
||||
</fdm_config>
|
||||
|
|
|
|||
399
A320-200-CFM.xml
399
A320-200-CFM.xml
|
|
@ -581,389 +581,20 @@ YAW MOI_________3950000______23089847_______24848934
|
|||
|
||||
<flight_control name="none"/>
|
||||
|
||||
<aerodynamics>
|
||||
<aerodynamics file="Systems/a320-aerodynamics.xml" />
|
||||
|
||||
<axis name="LIFT">
|
||||
|
||||
<function name="aero/force/Lift_alpha">
|
||||
<description>Lift due to alpha</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">aero/alpha-rad</independentVar>
|
||||
<tableData>
|
||||
-0.20 -0.900
|
||||
0.00 0.103
|
||||
0.15 1.600
|
||||
0.23 1.900
|
||||
0.60 1.000
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Lift_flap">
|
||||
<description>Delta Lift due to flaps</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">fcs/flap-pos-norm</independentVar>
|
||||
<tableData>
|
||||
0.000 0.00000
|
||||
0.290 0.00250
|
||||
0.596 0.00700
|
||||
0.645 0.01300
|
||||
1.000 0.01700
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Lift_slats">
|
||||
<description>Delta Lift due to slats</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/slat-pos-deg</property>
|
||||
<value> 0.01000 </value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Lift_speedbrake">
|
||||
<description>Delta Lift due to speedbrake</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/speedbrake-pos-norm</property>
|
||||
<value>-0.15</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Lift_elevator">
|
||||
<description>Lift due to Elevator Deflection</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/elevator-pos-rad</property>
|
||||
<value>0.04</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="DRAG">
|
||||
|
||||
<function name="aero/force/Drag_basic">
|
||||
<description>Drag at zero lift</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">aero/alpha-rad</independentVar>
|
||||
<tableData>
|
||||
-1.57 1.260
|
||||
-0.26 0.018
|
||||
0.00 0.008
|
||||
0.26 0.017
|
||||
1.57 1.320
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_induced">
|
||||
<description>Induced drag</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>aero/cl-squared</property>
|
||||
<value>0.035</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_mach">
|
||||
<description>Drag due to mach</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<tableData>
|
||||
0.00 0.000
|
||||
0.79 0.000
|
||||
1.10 0.023
|
||||
1.80 0.015
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_flap">
|
||||
<description>Drag due to flaps</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/flap-pos-deg</property>
|
||||
<value> 0.00090 </value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_slats">
|
||||
<description>Drag due to slats</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/flap-pos-deg</property>
|
||||
<value> 0.00120 </value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_gear">
|
||||
<description>Drag due to gear</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>gear/gear-pos-norm</property>
|
||||
<value>0.025</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_speedbrake">
|
||||
<description>Drag due to speedbrakes</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/speedbrake-pos-norm</property>
|
||||
<value>0.035</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_beta">
|
||||
<description>Drag due to sideslip</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">aero/beta-rad</independentVar>
|
||||
<tableData>
|
||||
-1.57 1.230
|
||||
-0.26 0.050
|
||||
0.00 0.000
|
||||
0.26 0.050
|
||||
1.57 1.230
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_elevator">
|
||||
<description>Drag due to Elevator Deflection</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<abs><property>fcs/elevator-pos-norm</property></abs>
|
||||
<value>0.035</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="SIDE">
|
||||
|
||||
<function name="aero/force/Side_beta">
|
||||
<description>Side force due to beta</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>aero/beta-rad</property>
|
||||
<value>-1</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="ROLL">
|
||||
|
||||
<function name="aero/moment/Roll_beta">
|
||||
<description>Roll moment due to beta</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/beta-rad</property>
|
||||
<value>-0.1</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Roll_damp">
|
||||
<description>Roll moment due to roll rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/bi2vel</property>
|
||||
<property>velocities/p-aero-rad_sec</property>
|
||||
<value>-0.95</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Roll_yaw">
|
||||
<description>Roll moment due to yaw rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/bi2vel</property>
|
||||
<property>velocities/r-aero-rad_sec</property>
|
||||
<value>0.005</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Roll_aileron">
|
||||
<description>Roll moment due to aileron</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>fcs/left-aileron-pos-rad</property>
|
||||
<value>0.20</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Roll_rudder">
|
||||
<description>Roll moment due to rudder</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>fcs/rudder-pos-rad</property>
|
||||
<value>0.003</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="PITCH">
|
||||
|
||||
<function name="aero/moment/Pitch_alpha">
|
||||
<description>Pitch moment due to alpha</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/cbarw-ft</property>
|
||||
<property>aero/alpha-rad</property>
|
||||
<value>-0.6</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Pitch_elevator">
|
||||
<description>Pitch moment due to elevator</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/cbarw-ft</property>
|
||||
<property>fcs/elevator-pos-rad</property>
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<tableData>
|
||||
0.0 -1.900
|
||||
2.0 -0.900
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Pitch_damp">
|
||||
<description>Pitch moment due to pitch rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/cbarw-ft</property>
|
||||
<property>aero/ci2vel</property>
|
||||
<property>velocities/q-aero-rad_sec</property>
|
||||
<value>-140</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Pitch_alphadot">
|
||||
<description>Pitch moment due to alpha rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/cbarw-ft</property>
|
||||
<property>aero/ci2vel</property>
|
||||
<property>aero/alphadot-rad_sec</property>
|
||||
<value>-1</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="YAW">
|
||||
|
||||
<function name="aero/moment/Yaw_beta">
|
||||
<description>Yaw moment due to beta</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/beta-rad</property>
|
||||
<value>0.12</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Yaw_damp">
|
||||
<description>Yaw moment due to yaw rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/bi2vel</property>
|
||||
<property>velocities/r-aero-rad_sec</property>
|
||||
<value>-0.2</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Yaw_rudder">
|
||||
<description>Yaw moment due to rudder</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>fcs/rudder-pos-rad</property>
|
||||
<value>-0.2</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Yaw_aileron">
|
||||
<description>Adverse yaw</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>fcs/left-aileron-pos-rad</property>
|
||||
<value>0</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
</aerodynamics>
|
||||
|
||||
<external_reactions>
|
||||
<force name="pushback" frame="BODY">
|
||||
<location unit="IN">
|
||||
<x>294</x>
|
||||
<y>0</y>
|
||||
<z>-149</z>
|
||||
</location>
|
||||
<direction>
|
||||
<x>1</x>
|
||||
<y>0</y>
|
||||
<z>0</z>
|
||||
</direction>
|
||||
</force>
|
||||
</external_reactions>
|
||||
<external_reactions>
|
||||
<force name="pushback" frame="BODY">
|
||||
<location unit="IN">
|
||||
<x>294</x>
|
||||
<y>0</y>
|
||||
<z>-149</z>
|
||||
</location>
|
||||
<direction>
|
||||
<x>1</x>
|
||||
<y>0</y>
|
||||
<z>0</z>
|
||||
</direction>
|
||||
</force>
|
||||
</external_reactions>
|
||||
</fdm_config>
|
||||
|
|
|
|||
401
A320-200-IAE.xml
401
A320-200-IAE.xml
|
|
@ -580,390 +580,21 @@ YAW MOI_________3950000______23089847_______24848934
|
|||
<system file="fcs" />
|
||||
|
||||
<flight_control name="none"/>
|
||||
|
||||
<aerodynamics file="Systems/a320-aerodynamics.xml" />
|
||||
|
||||
<aerodynamics>
|
||||
|
||||
<axis name="LIFT">
|
||||
|
||||
<function name="aero/force/Lift_alpha">
|
||||
<description>Lift due to alpha</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">aero/alpha-rad</independentVar>
|
||||
<tableData>
|
||||
-0.20 -0.900
|
||||
0.00 0.103
|
||||
0.15 1.600
|
||||
0.23 1.900
|
||||
0.60 1.000
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Lift_flap">
|
||||
<description>Delta Lift due to flaps</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">fcs/flap-pos-norm</independentVar>
|
||||
<tableData>
|
||||
0.000 0.00000
|
||||
0.290 0.00250
|
||||
0.596 0.00700
|
||||
0.645 0.01300
|
||||
1.000 0.01700
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Lift_slats">
|
||||
<description>Delta Lift due to slats</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/slat-pos-deg</property>
|
||||
<value> 0.01000 </value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Lift_speedbrake">
|
||||
<description>Delta Lift due to speedbrake</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/speedbrake-pos-norm</property>
|
||||
<value>-0.15</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Lift_elevator">
|
||||
<description>Lift due to Elevator Deflection</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/elevator-pos-rad</property>
|
||||
<value>0.04</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="DRAG">
|
||||
|
||||
<function name="aero/force/Drag_basic">
|
||||
<description>Drag at zero lift</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">aero/alpha-rad</independentVar>
|
||||
<tableData>
|
||||
-1.57 1.260
|
||||
-0.26 0.018
|
||||
0.00 0.008
|
||||
0.26 0.017
|
||||
1.57 1.320
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_induced">
|
||||
<description>Induced drag</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>aero/cl-squared</property>
|
||||
<value>0.035</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_mach">
|
||||
<description>Drag due to mach</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<tableData>
|
||||
0.00 0.000
|
||||
0.79 0.000
|
||||
1.10 0.023
|
||||
1.80 0.015
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_flap">
|
||||
<description>Drag due to flaps</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/flap-pos-deg</property>
|
||||
<value> 0.00090 </value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_slats">
|
||||
<description>Drag due to slats</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/flap-pos-deg</property>
|
||||
<value> 0.00120 </value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_gear">
|
||||
<description>Drag due to gear</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>gear/gear-pos-norm</property>
|
||||
<value>0.025</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_speedbrake">
|
||||
<description>Drag due to speedbrakes</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/speedbrake-pos-norm</property>
|
||||
<value>0.035</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_beta">
|
||||
<description>Drag due to sideslip</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">aero/beta-rad</independentVar>
|
||||
<tableData>
|
||||
-1.57 1.230
|
||||
-0.26 0.050
|
||||
0.00 0.000
|
||||
0.26 0.050
|
||||
1.57 1.230
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_elevator">
|
||||
<description>Drag due to Elevator Deflection</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<abs><property>fcs/elevator-pos-norm</property></abs>
|
||||
<value>0.035</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="SIDE">
|
||||
|
||||
<function name="aero/force/Side_beta">
|
||||
<description>Side force due to beta</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>aero/beta-rad</property>
|
||||
<value>-1</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="ROLL">
|
||||
|
||||
<function name="aero/moment/Roll_beta">
|
||||
<description>Roll moment due to beta</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/beta-rad</property>
|
||||
<value>-0.1</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Roll_damp">
|
||||
<description>Roll moment due to roll rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/bi2vel</property>
|
||||
<property>velocities/p-aero-rad_sec</property>
|
||||
<value>-0.95</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Roll_yaw">
|
||||
<description>Roll moment due to yaw rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/bi2vel</property>
|
||||
<property>velocities/r-aero-rad_sec</property>
|
||||
<value>0.005</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Roll_aileron">
|
||||
<description>Roll moment due to aileron</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>fcs/left-aileron-pos-rad</property>
|
||||
<value>0.20</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Roll_rudder">
|
||||
<description>Roll moment due to rudder</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>fcs/rudder-pos-rad</property>
|
||||
<value>0.003</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="PITCH">
|
||||
|
||||
<function name="aero/moment/Pitch_alpha">
|
||||
<description>Pitch moment due to alpha</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/cbarw-ft</property>
|
||||
<property>aero/alpha-rad</property>
|
||||
<value>-0.6</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Pitch_elevator">
|
||||
<description>Pitch moment due to elevator</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/cbarw-ft</property>
|
||||
<property>fcs/elevator-pos-rad</property>
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<tableData>
|
||||
0.0 -1.900
|
||||
2.0 -0.900
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Pitch_damp">
|
||||
<description>Pitch moment due to pitch rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/cbarw-ft</property>
|
||||
<property>aero/ci2vel</property>
|
||||
<property>velocities/q-aero-rad_sec</property>
|
||||
<value>-140</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Pitch_alphadot">
|
||||
<description>Pitch moment due to alpha rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/cbarw-ft</property>
|
||||
<property>aero/ci2vel</property>
|
||||
<property>aero/alphadot-rad_sec</property>
|
||||
<value>-1</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="YAW">
|
||||
|
||||
<function name="aero/moment/Yaw_beta">
|
||||
<description>Yaw moment due to beta</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/beta-rad</property>
|
||||
<value>0.12</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Yaw_damp">
|
||||
<description>Yaw moment due to yaw rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/bi2vel</property>
|
||||
<property>velocities/r-aero-rad_sec</property>
|
||||
<value>-0.2</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Yaw_rudder">
|
||||
<description>Yaw moment due to rudder</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>fcs/rudder-pos-rad</property>
|
||||
<value>-0.2</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Yaw_aileron">
|
||||
<description>Adverse yaw</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>fcs/left-aileron-pos-rad</property>
|
||||
<value>0</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
</aerodynamics>
|
||||
|
||||
<external_reactions>
|
||||
<force name="pushback" frame="BODY">
|
||||
<location unit="IN">
|
||||
<x>294</x>
|
||||
<y>0</y>
|
||||
<z>-149</z>
|
||||
</location>
|
||||
<direction>
|
||||
<x>1</x>
|
||||
<y>0</y>
|
||||
<z>0</z>
|
||||
</direction>
|
||||
</force>
|
||||
</external_reactions>
|
||||
<external_reactions>
|
||||
<force name="pushback" frame="BODY">
|
||||
<location unit="IN">
|
||||
<x>294</x>
|
||||
<y>0</y>
|
||||
<z>-149</z>
|
||||
</location>
|
||||
<direction>
|
||||
<x>1</x>
|
||||
<y>0</y>
|
||||
<z>0</z>
|
||||
</direction>
|
||||
</force>
|
||||
</external_reactions>
|
||||
</fdm_config>
|
||||
|
|
|
|||
399
A321-200-CFM.xml
399
A321-200-CFM.xml
|
|
@ -581,389 +581,20 @@ YAW MOI_________3950000______23089847_______24848934
|
|||
|
||||
<flight_control name="none"/>
|
||||
|
||||
<aerodynamics>
|
||||
<aerodynamics file="Systems/a321-aerodynamics.xml" />
|
||||
|
||||
<axis name="LIFT">
|
||||
|
||||
<function name="aero/force/Lift_alpha">
|
||||
<description>Lift due to alpha</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">aero/alpha-rad</independentVar>
|
||||
<tableData>
|
||||
-0.20 -0.900
|
||||
0.00 0.103
|
||||
0.15 1.600
|
||||
0.23 1.900
|
||||
0.60 1.000
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Lift_flap">
|
||||
<description>Delta Lift due to flaps</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">fcs/flap-pos-norm</independentVar>
|
||||
<tableData>
|
||||
0.000 0.00000
|
||||
0.290 0.00250
|
||||
0.596 0.00700
|
||||
0.645 0.01300
|
||||
1.000 0.01700
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Lift_slats">
|
||||
<description>Delta Lift due to slats</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/slat-pos-deg</property>
|
||||
<value> 0.01000 </value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Lift_speedbrake">
|
||||
<description>Delta Lift due to speedbrake</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/speedbrake-pos-norm</property>
|
||||
<value>-0.15</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Lift_elevator">
|
||||
<description>Lift due to Elevator Deflection</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/elevator-pos-rad</property>
|
||||
<value>0.04</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="DRAG">
|
||||
|
||||
<function name="aero/force/Drag_basic">
|
||||
<description>Drag at zero lift</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">aero/alpha-rad</independentVar>
|
||||
<tableData>
|
||||
-1.57 1.260
|
||||
-0.26 0.018
|
||||
0.00 0.008
|
||||
0.26 0.017
|
||||
1.57 1.320
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_induced">
|
||||
<description>Induced drag</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>aero/cl-squared</property>
|
||||
<value>0.035</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_mach">
|
||||
<description>Drag due to mach</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<tableData>
|
||||
0.00 0.000
|
||||
0.79 0.000
|
||||
1.10 0.023
|
||||
1.80 0.015
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_flap">
|
||||
<description>Drag due to flaps</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/flap-pos-deg</property>
|
||||
<value> 0.00090 </value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_slats">
|
||||
<description>Drag due to slats</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/flap-pos-deg</property>
|
||||
<value> 0.00120 </value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_gear">
|
||||
<description>Drag due to gear</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>gear/gear-pos-norm</property>
|
||||
<value>0.025</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_speedbrake">
|
||||
<description>Drag due to speedbrakes</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/speedbrake-pos-norm</property>
|
||||
<value>0.035</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_beta">
|
||||
<description>Drag due to sideslip</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">aero/beta-rad</independentVar>
|
||||
<tableData>
|
||||
-1.57 1.230
|
||||
-0.26 0.050
|
||||
0.00 0.000
|
||||
0.26 0.050
|
||||
1.57 1.230
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_elevator">
|
||||
<description>Drag due to Elevator Deflection</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<abs><property>fcs/elevator-pos-norm</property></abs>
|
||||
<value>0.035</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="SIDE">
|
||||
|
||||
<function name="aero/force/Side_beta">
|
||||
<description>Side force due to beta</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>aero/beta-rad</property>
|
||||
<value>-1</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="ROLL">
|
||||
|
||||
<function name="aero/moment/Roll_beta">
|
||||
<description>Roll moment due to beta</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/beta-rad</property>
|
||||
<value>-0.1</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Roll_damp">
|
||||
<description>Roll moment due to roll rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/bi2vel</property>
|
||||
<property>velocities/p-aero-rad_sec</property>
|
||||
<value>-0.95</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Roll_yaw">
|
||||
<description>Roll moment due to yaw rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/bi2vel</property>
|
||||
<property>velocities/r-aero-rad_sec</property>
|
||||
<value>0.005</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Roll_aileron">
|
||||
<description>Roll moment due to aileron</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>fcs/left-aileron-pos-rad</property>
|
||||
<value>0.20</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Roll_rudder">
|
||||
<description>Roll moment due to rudder</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>fcs/rudder-pos-rad</property>
|
||||
<value>0.003</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="PITCH">
|
||||
|
||||
<function name="aero/moment/Pitch_alpha">
|
||||
<description>Pitch moment due to alpha</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/cbarw-ft</property>
|
||||
<property>aero/alpha-rad</property>
|
||||
<value>-0.6</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Pitch_elevator">
|
||||
<description>Pitch moment due to elevator</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/cbarw-ft</property>
|
||||
<property>fcs/elevator-pos-rad</property>
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<tableData>
|
||||
0.0 -1.900
|
||||
2.0 -0.900
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Pitch_damp">
|
||||
<description>Pitch moment due to pitch rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/cbarw-ft</property>
|
||||
<property>aero/ci2vel</property>
|
||||
<property>velocities/q-aero-rad_sec</property>
|
||||
<value>-140</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Pitch_alphadot">
|
||||
<description>Pitch moment due to alpha rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/cbarw-ft</property>
|
||||
<property>aero/ci2vel</property>
|
||||
<property>aero/alphadot-rad_sec</property>
|
||||
<value>-1</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="YAW">
|
||||
|
||||
<function name="aero/moment/Yaw_beta">
|
||||
<description>Yaw moment due to beta</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/beta-rad</property>
|
||||
<value>0.12</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Yaw_damp">
|
||||
<description>Yaw moment due to yaw rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/bi2vel</property>
|
||||
<property>velocities/r-aero-rad_sec</property>
|
||||
<value>-0.2</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Yaw_rudder">
|
||||
<description>Yaw moment due to rudder</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>fcs/rudder-pos-rad</property>
|
||||
<value>-0.2</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Yaw_aileron">
|
||||
<description>Adverse yaw</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>fcs/left-aileron-pos-rad</property>
|
||||
<value>0</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
</aerodynamics>
|
||||
|
||||
<external_reactions>
|
||||
<force name="pushback" frame="BODY">
|
||||
<location unit="IN">
|
||||
<x>294</x>
|
||||
<y>0</y>
|
||||
<z>-149</z>
|
||||
</location>
|
||||
<direction>
|
||||
<x>1</x>
|
||||
<y>0</y>
|
||||
<z>0</z>
|
||||
</direction>
|
||||
</force>
|
||||
</external_reactions>
|
||||
<external_reactions>
|
||||
<force name="pushback" frame="BODY">
|
||||
<location unit="IN">
|
||||
<x>294</x>
|
||||
<y>0</y>
|
||||
<z>-149</z>
|
||||
</location>
|
||||
<direction>
|
||||
<x>1</x>
|
||||
<y>0</y>
|
||||
<z>0</z>
|
||||
</direction>
|
||||
</force>
|
||||
</external_reactions>
|
||||
</fdm_config>
|
||||
|
|
|
|||
401
A321-200-IAE.xml
401
A321-200-IAE.xml
|
|
@ -579,391 +579,22 @@ YAW MOI_________3950000______23089847_______24848934
|
|||
<system file="fmgc" />
|
||||
<system file="fcs" />
|
||||
|
||||
<flight_control name="none"/>
|
||||
<flight_control name="none" />
|
||||
|
||||
<aerodynamics>
|
||||
<aerodynamics file="Systems/a321-aerodynamics.xml" />
|
||||
|
||||
<axis name="LIFT">
|
||||
|
||||
<function name="aero/force/Lift_alpha">
|
||||
<description>Lift due to alpha</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">aero/alpha-rad</independentVar>
|
||||
<tableData>
|
||||
-0.20 -0.900
|
||||
0.00 0.103
|
||||
0.15 1.600
|
||||
0.23 1.900
|
||||
0.60 1.000
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Lift_flap">
|
||||
<description>Delta Lift due to flaps</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">fcs/flap-pos-norm</independentVar>
|
||||
<tableData>
|
||||
0.000 0.00000
|
||||
0.290 0.00250
|
||||
0.596 0.00700
|
||||
0.645 0.01300
|
||||
1.000 0.01700
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Lift_slats">
|
||||
<description>Delta Lift due to slats</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/slat-pos-deg</property>
|
||||
<value> 0.01000 </value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Lift_speedbrake">
|
||||
<description>Delta Lift due to speedbrake</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/speedbrake-pos-norm</property>
|
||||
<value>-0.15</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Lift_elevator">
|
||||
<description>Lift due to Elevator Deflection</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/elevator-pos-rad</property>
|
||||
<value>0.04</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="DRAG">
|
||||
|
||||
<function name="aero/force/Drag_basic">
|
||||
<description>Drag at zero lift</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">aero/alpha-rad</independentVar>
|
||||
<tableData>
|
||||
-1.57 1.260
|
||||
-0.26 0.018
|
||||
0.00 0.008
|
||||
0.26 0.017
|
||||
1.57 1.320
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_induced">
|
||||
<description>Induced drag</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>aero/cl-squared</property>
|
||||
<value>0.035</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_mach">
|
||||
<description>Drag due to mach</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<tableData>
|
||||
0.00 0.000
|
||||
0.79 0.000
|
||||
1.10 0.023
|
||||
1.80 0.015
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_flap">
|
||||
<description>Drag due to flaps</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/flap-pos-deg</property>
|
||||
<value> 0.00090 </value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_slats">
|
||||
<description>Drag due to slats</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/flap-pos-deg</property>
|
||||
<value> 0.00120 </value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_gear">
|
||||
<description>Drag due to gear</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>gear/gear-pos-norm</property>
|
||||
<value>0.025</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_speedbrake">
|
||||
<description>Drag due to speedbrakes</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/speedbrake-pos-norm</property>
|
||||
<value>0.035</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_beta">
|
||||
<description>Drag due to sideslip</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">aero/beta-rad</independentVar>
|
||||
<tableData>
|
||||
-1.57 1.230
|
||||
-0.26 0.050
|
||||
0.00 0.000
|
||||
0.26 0.050
|
||||
1.57 1.230
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_elevator">
|
||||
<description>Drag due to Elevator Deflection</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<abs><property>fcs/elevator-pos-norm</property></abs>
|
||||
<value>0.035</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="SIDE">
|
||||
|
||||
<function name="aero/force/Side_beta">
|
||||
<description>Side force due to beta</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>aero/beta-rad</property>
|
||||
<value>-1</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="ROLL">
|
||||
|
||||
<function name="aero/moment/Roll_beta">
|
||||
<description>Roll moment due to beta</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/beta-rad</property>
|
||||
<value>-0.1</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Roll_damp">
|
||||
<description>Roll moment due to roll rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/bi2vel</property>
|
||||
<property>velocities/p-aero-rad_sec</property>
|
||||
<value>-0.95</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Roll_yaw">
|
||||
<description>Roll moment due to yaw rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/bi2vel</property>
|
||||
<property>velocities/r-aero-rad_sec</property>
|
||||
<value>0.005</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Roll_aileron">
|
||||
<description>Roll moment due to aileron</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>fcs/left-aileron-pos-rad</property>
|
||||
<value>0.20</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Roll_rudder">
|
||||
<description>Roll moment due to rudder</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>fcs/rudder-pos-rad</property>
|
||||
<value>0.003</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="PITCH">
|
||||
|
||||
<function name="aero/moment/Pitch_alpha">
|
||||
<description>Pitch moment due to alpha</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/cbarw-ft</property>
|
||||
<property>aero/alpha-rad</property>
|
||||
<value>-0.6</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Pitch_elevator">
|
||||
<description>Pitch moment due to elevator</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/cbarw-ft</property>
|
||||
<property>fcs/elevator-pos-rad</property>
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<tableData>
|
||||
0.0 -1.900
|
||||
2.0 -0.900
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Pitch_damp">
|
||||
<description>Pitch moment due to pitch rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/cbarw-ft</property>
|
||||
<property>aero/ci2vel</property>
|
||||
<property>velocities/q-aero-rad_sec</property>
|
||||
<value>-140</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Pitch_alphadot">
|
||||
<description>Pitch moment due to alpha rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/cbarw-ft</property>
|
||||
<property>aero/ci2vel</property>
|
||||
<property>aero/alphadot-rad_sec</property>
|
||||
<value>-1</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="YAW">
|
||||
|
||||
<function name="aero/moment/Yaw_beta">
|
||||
<description>Yaw moment due to beta</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/beta-rad</property>
|
||||
<value>0.12</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Yaw_damp">
|
||||
<description>Yaw moment due to yaw rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/bi2vel</property>
|
||||
<property>velocities/r-aero-rad_sec</property>
|
||||
<value>-0.2</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Yaw_rudder">
|
||||
<description>Yaw moment due to rudder</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>fcs/rudder-pos-rad</property>
|
||||
<value>-0.2</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Yaw_aileron">
|
||||
<description>Adverse yaw</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>fcs/left-aileron-pos-rad</property>
|
||||
<value>0</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
</aerodynamics>
|
||||
|
||||
<external_reactions>
|
||||
<force name="pushback" frame="BODY">
|
||||
<location unit="IN">
|
||||
<x>294</x>
|
||||
<y>0</y>
|
||||
<z>-149</z>
|
||||
</location>
|
||||
<direction>
|
||||
<x>1</x>
|
||||
<y>0</y>
|
||||
<z>0</z>
|
||||
</direction>
|
||||
</force>
|
||||
</external_reactions>
|
||||
<external_reactions>
|
||||
<force name="pushback" frame="BODY">
|
||||
<location unit="IN">
|
||||
<x>294</x>
|
||||
<y>0</y>
|
||||
<z>-149</z>
|
||||
</location>
|
||||
<direction>
|
||||
<x>1</x>
|
||||
<y>0</y>
|
||||
<z>0</z>
|
||||
</direction>
|
||||
</force>
|
||||
</external_reactions>
|
||||
</fdm_config>
|
||||
|
|
|
|||
371
Systems/a319-aerodynamics.xml
Normal file
371
Systems/a319-aerodynamics.xml
Normal file
|
|
@ -0,0 +1,371 @@
|
|||
<!-- A3XX Aerodynamics -->
|
||||
<!-- Joshua Davidson (it0uchpods) -->
|
||||
|
||||
<aerodynamics>
|
||||
<axis name="LIFT">
|
||||
|
||||
<function name="aero/force/Lift_alpha">
|
||||
<description>Lift due to alpha</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">aero/alpha-rad</independentVar>
|
||||
<tableData>
|
||||
-0.20 -0.900
|
||||
0.00 0.103
|
||||
0.15 1.600
|
||||
0.23 1.900
|
||||
0.60 1.000
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Lift_flap">
|
||||
<description>Delta Lift due to flaps</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">fcs/flap-pos-norm</independentVar>
|
||||
<tableData>
|
||||
0.000 0.00000
|
||||
0.290 0.00250
|
||||
0.596 0.00700
|
||||
0.645 0.01300
|
||||
1.000 0.01700
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Lift_slats">
|
||||
<description>Delta Lift due to slats</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/slat-pos-deg</property>
|
||||
<value> 0.01000 </value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Lift_speedbrake">
|
||||
<description>Delta Lift due to speedbrake</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/speedbrake-pos-norm</property>
|
||||
<value>-0.15</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Lift_elevator">
|
||||
<description>Lift due to Elevator Deflection</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/elevator-pos-rad</property>
|
||||
<value>0.04</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="DRAG">
|
||||
|
||||
<function name="aero/force/Drag_basic">
|
||||
<description>Drag at zero lift</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">aero/alpha-rad</independentVar>
|
||||
<tableData>
|
||||
-1.57 1.260
|
||||
-0.26 0.018
|
||||
0.00 0.008
|
||||
0.26 0.017
|
||||
1.57 1.320
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_induced">
|
||||
<description>Induced drag</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>aero/cl-squared</property>
|
||||
<value>0.035</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_mach">
|
||||
<description>Drag due to mach</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<tableData>
|
||||
0.00 0.000
|
||||
0.79 0.000
|
||||
1.10 0.023
|
||||
1.80 0.015
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_flap">
|
||||
<description>Drag due to flaps</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/flap-pos-deg</property>
|
||||
<value> 0.00080 </value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_slats">
|
||||
<description>Drag due to slats</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/flap-pos-deg</property>
|
||||
<value> 0.00080 </value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_gear">
|
||||
<description>Drag due to gear</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>gear/gear-pos-norm</property>
|
||||
<value>0.025</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_speedbrake">
|
||||
<description>Drag due to speedbrakes</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/speedbrake-pos-norm</property>
|
||||
<value>0.035</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_beta">
|
||||
<description>Drag due to sideslip</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">aero/beta-rad</independentVar>
|
||||
<tableData>
|
||||
-1.57 1.230
|
||||
-0.26 0.050
|
||||
0.00 0.000
|
||||
0.26 0.050
|
||||
1.57 1.230
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_elevator">
|
||||
<description>Drag due to Elevator Deflection</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<abs><property>fcs/elevator-pos-norm</property></abs>
|
||||
<value>0.035</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="SIDE">
|
||||
|
||||
<function name="aero/force/Side_beta">
|
||||
<description>Side force due to beta</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>aero/beta-rad</property>
|
||||
<value>-1</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="ROLL">
|
||||
|
||||
<function name="aero/moment/Roll_beta">
|
||||
<description>Roll moment due to beta</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/beta-rad</property>
|
||||
<value>-0.1</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Roll_damp">
|
||||
<description>Roll moment due to roll rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/bi2vel</property>
|
||||
<property>velocities/p-aero-rad_sec</property>
|
||||
<value>-0.95</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Roll_yaw">
|
||||
<description>Roll moment due to yaw rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/bi2vel</property>
|
||||
<property>velocities/r-aero-rad_sec</property>
|
||||
<value>0.005</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Roll_aileron">
|
||||
<description>Roll moment due to aileron</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>fcs/left-aileron-pos-rad</property>
|
||||
<value>0.20</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Roll_rudder">
|
||||
<description>Roll moment due to rudder</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>fcs/rudder-pos-rad</property>
|
||||
<value>0.003</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="PITCH">
|
||||
|
||||
<function name="aero/moment/Pitch_alpha">
|
||||
<description>Pitch moment due to alpha</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/cbarw-ft</property>
|
||||
<property>aero/alpha-rad</property>
|
||||
<value>-0.6</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Pitch_elevator">
|
||||
<description>Pitch moment due to elevator</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/cbarw-ft</property>
|
||||
<property>fcs/elevator-pos-rad</property>
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<tableData>
|
||||
0.0 -1.900
|
||||
2.0 -0.900
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Pitch_damp">
|
||||
<description>Pitch moment due to pitch rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/cbarw-ft</property>
|
||||
<property>aero/ci2vel</property>
|
||||
<property>velocities/q-aero-rad_sec</property>
|
||||
<value>-140</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Pitch_alphadot">
|
||||
<description>Pitch moment due to alpha rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/cbarw-ft</property>
|
||||
<property>aero/ci2vel</property>
|
||||
<property>aero/alphadot-rad_sec</property>
|
||||
<value>-1</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="YAW">
|
||||
|
||||
<function name="aero/moment/Yaw_beta">
|
||||
<description>Yaw moment due to beta</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/beta-rad</property>
|
||||
<value>0.12</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Yaw_damp">
|
||||
<description>Yaw moment due to yaw rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/bi2vel</property>
|
||||
<property>velocities/r-aero-rad_sec</property>
|
||||
<value>-0.2</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Yaw_rudder">
|
||||
<description>Yaw moment due to rudder</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>fcs/rudder-pos-rad</property>
|
||||
<value>-0.2</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Yaw_aileron">
|
||||
<description>Adverse yaw</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>fcs/left-aileron-pos-rad</property>
|
||||
<value>0</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
</aerodynamics>
|
||||
371
Systems/a320-aerodynamics.xml
Normal file
371
Systems/a320-aerodynamics.xml
Normal file
|
|
@ -0,0 +1,371 @@
|
|||
<!-- A3XX Aerodynamics -->
|
||||
<!-- Joshua Davidson (it0uchpods) -->
|
||||
|
||||
<aerodynamics>
|
||||
<axis name="LIFT">
|
||||
|
||||
<function name="aero/force/Lift_alpha">
|
||||
<description>Lift due to alpha</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">aero/alpha-rad</independentVar>
|
||||
<tableData>
|
||||
-0.20 -0.900
|
||||
0.00 0.103
|
||||
0.15 1.600
|
||||
0.23 1.900
|
||||
0.60 1.000
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Lift_flap">
|
||||
<description>Delta Lift due to flaps</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">fcs/flap-pos-norm</independentVar>
|
||||
<tableData>
|
||||
0.000 0.00000
|
||||
0.290 0.00250
|
||||
0.596 0.00700
|
||||
0.645 0.01300
|
||||
1.000 0.01700
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Lift_slats">
|
||||
<description>Delta Lift due to slats</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/slat-pos-deg</property>
|
||||
<value> 0.01000 </value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Lift_speedbrake">
|
||||
<description>Delta Lift due to speedbrake</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/speedbrake-pos-norm</property>
|
||||
<value>-0.15</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Lift_elevator">
|
||||
<description>Lift due to Elevator Deflection</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/elevator-pos-rad</property>
|
||||
<value>0.04</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="DRAG">
|
||||
|
||||
<function name="aero/force/Drag_basic">
|
||||
<description>Drag at zero lift</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">aero/alpha-rad</independentVar>
|
||||
<tableData>
|
||||
-1.57 1.260
|
||||
-0.26 0.018
|
||||
0.00 0.008
|
||||
0.26 0.017
|
||||
1.57 1.320
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_induced">
|
||||
<description>Induced drag</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>aero/cl-squared</property>
|
||||
<value>0.035</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_mach">
|
||||
<description>Drag due to mach</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<tableData>
|
||||
0.00 0.000
|
||||
0.79 0.000
|
||||
1.10 0.023
|
||||
1.80 0.015
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_flap">
|
||||
<description>Drag due to flaps</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/flap-pos-deg</property>
|
||||
<value> 0.00080 </value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_slats">
|
||||
<description>Drag due to slats</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/flap-pos-deg</property>
|
||||
<value> 0.00080 </value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_gear">
|
||||
<description>Drag due to gear</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>gear/gear-pos-norm</property>
|
||||
<value>0.025</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_speedbrake">
|
||||
<description>Drag due to speedbrakes</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/speedbrake-pos-norm</property>
|
||||
<value>0.035</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_beta">
|
||||
<description>Drag due to sideslip</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">aero/beta-rad</independentVar>
|
||||
<tableData>
|
||||
-1.57 1.230
|
||||
-0.26 0.050
|
||||
0.00 0.000
|
||||
0.26 0.050
|
||||
1.57 1.230
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_elevator">
|
||||
<description>Drag due to Elevator Deflection</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<abs><property>fcs/elevator-pos-norm</property></abs>
|
||||
<value>0.035</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="SIDE">
|
||||
|
||||
<function name="aero/force/Side_beta">
|
||||
<description>Side force due to beta</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>aero/beta-rad</property>
|
||||
<value>-1</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="ROLL">
|
||||
|
||||
<function name="aero/moment/Roll_beta">
|
||||
<description>Roll moment due to beta</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/beta-rad</property>
|
||||
<value>-0.1</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Roll_damp">
|
||||
<description>Roll moment due to roll rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/bi2vel</property>
|
||||
<property>velocities/p-aero-rad_sec</property>
|
||||
<value>-0.95</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Roll_yaw">
|
||||
<description>Roll moment due to yaw rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/bi2vel</property>
|
||||
<property>velocities/r-aero-rad_sec</property>
|
||||
<value>0.005</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Roll_aileron">
|
||||
<description>Roll moment due to aileron</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>fcs/left-aileron-pos-rad</property>
|
||||
<value>0.20</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Roll_rudder">
|
||||
<description>Roll moment due to rudder</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>fcs/rudder-pos-rad</property>
|
||||
<value>0.003</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="PITCH">
|
||||
|
||||
<function name="aero/moment/Pitch_alpha">
|
||||
<description>Pitch moment due to alpha</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/cbarw-ft</property>
|
||||
<property>aero/alpha-rad</property>
|
||||
<value>-0.6</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Pitch_elevator">
|
||||
<description>Pitch moment due to elevator</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/cbarw-ft</property>
|
||||
<property>fcs/elevator-pos-rad</property>
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<tableData>
|
||||
0.0 -1.900
|
||||
2.0 -0.900
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Pitch_damp">
|
||||
<description>Pitch moment due to pitch rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/cbarw-ft</property>
|
||||
<property>aero/ci2vel</property>
|
||||
<property>velocities/q-aero-rad_sec</property>
|
||||
<value>-140</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Pitch_alphadot">
|
||||
<description>Pitch moment due to alpha rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/cbarw-ft</property>
|
||||
<property>aero/ci2vel</property>
|
||||
<property>aero/alphadot-rad_sec</property>
|
||||
<value>-1</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="YAW">
|
||||
|
||||
<function name="aero/moment/Yaw_beta">
|
||||
<description>Yaw moment due to beta</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/beta-rad</property>
|
||||
<value>0.12</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Yaw_damp">
|
||||
<description>Yaw moment due to yaw rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/bi2vel</property>
|
||||
<property>velocities/r-aero-rad_sec</property>
|
||||
<value>-0.2</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Yaw_rudder">
|
||||
<description>Yaw moment due to rudder</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>fcs/rudder-pos-rad</property>
|
||||
<value>-0.2</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Yaw_aileron">
|
||||
<description>Adverse yaw</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>fcs/left-aileron-pos-rad</property>
|
||||
<value>0</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
</aerodynamics>
|
||||
371
Systems/a321-aerodynamics.xml
Normal file
371
Systems/a321-aerodynamics.xml
Normal file
|
|
@ -0,0 +1,371 @@
|
|||
<!-- A3XX Aerodynamics -->
|
||||
<!-- Joshua Davidson (it0uchpods) -->
|
||||
|
||||
<aerodynamics>
|
||||
<axis name="LIFT">
|
||||
|
||||
<function name="aero/force/Lift_alpha">
|
||||
<description>Lift due to alpha</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">aero/alpha-rad</independentVar>
|
||||
<tableData>
|
||||
-0.20 -0.900
|
||||
0.00 0.103
|
||||
0.15 1.600
|
||||
0.23 1.900
|
||||
0.60 1.000
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Lift_flap">
|
||||
<description>Delta Lift due to flaps</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">fcs/flap-pos-norm</independentVar>
|
||||
<tableData>
|
||||
0.000 0.00000
|
||||
0.290 0.00250
|
||||
0.596 0.00700
|
||||
0.645 0.01300
|
||||
1.000 0.01700
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Lift_slats">
|
||||
<description>Delta Lift due to slats</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/slat-pos-deg</property>
|
||||
<value> 0.01000 </value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Lift_speedbrake">
|
||||
<description>Delta Lift due to speedbrake</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/speedbrake-pos-norm</property>
|
||||
<value>-0.15</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Lift_elevator">
|
||||
<description>Lift due to Elevator Deflection</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/elevator-pos-rad</property>
|
||||
<value>0.04</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="DRAG">
|
||||
|
||||
<function name="aero/force/Drag_basic">
|
||||
<description>Drag at zero lift</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">aero/alpha-rad</independentVar>
|
||||
<tableData>
|
||||
-1.57 1.260
|
||||
-0.26 0.018
|
||||
0.00 0.008
|
||||
0.26 0.017
|
||||
1.57 1.320
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_induced">
|
||||
<description>Induced drag</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>aero/cl-squared</property>
|
||||
<value>0.035</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_mach">
|
||||
<description>Drag due to mach</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<tableData>
|
||||
0.00 0.000
|
||||
0.79 0.000
|
||||
1.10 0.023
|
||||
1.80 0.015
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_flap">
|
||||
<description>Drag due to flaps</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/flap-pos-deg</property>
|
||||
<value> 0.00080 </value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_slats">
|
||||
<description>Drag due to slats</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/flap-pos-deg</property>
|
||||
<value> 0.00080 </value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_gear">
|
||||
<description>Drag due to gear</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>gear/gear-pos-norm</property>
|
||||
<value>0.025</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_speedbrake">
|
||||
<description>Drag due to speedbrakes</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/speedbrake-pos-norm</property>
|
||||
<value>0.035</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_beta">
|
||||
<description>Drag due to sideslip</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">aero/beta-rad</independentVar>
|
||||
<tableData>
|
||||
-1.57 1.230
|
||||
-0.26 0.050
|
||||
0.00 0.000
|
||||
0.26 0.050
|
||||
1.57 1.230
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_elevator">
|
||||
<description>Drag due to Elevator Deflection</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<abs><property>fcs/elevator-pos-norm</property></abs>
|
||||
<value>0.035</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="SIDE">
|
||||
|
||||
<function name="aero/force/Side_beta">
|
||||
<description>Side force due to beta</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>aero/beta-rad</property>
|
||||
<value>-1</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="ROLL">
|
||||
|
||||
<function name="aero/moment/Roll_beta">
|
||||
<description>Roll moment due to beta</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/beta-rad</property>
|
||||
<value>-0.1</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Roll_damp">
|
||||
<description>Roll moment due to roll rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/bi2vel</property>
|
||||
<property>velocities/p-aero-rad_sec</property>
|
||||
<value>-0.95</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Roll_yaw">
|
||||
<description>Roll moment due to yaw rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/bi2vel</property>
|
||||
<property>velocities/r-aero-rad_sec</property>
|
||||
<value>0.005</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Roll_aileron">
|
||||
<description>Roll moment due to aileron</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>fcs/left-aileron-pos-rad</property>
|
||||
<value>0.20</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Roll_rudder">
|
||||
<description>Roll moment due to rudder</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>fcs/rudder-pos-rad</property>
|
||||
<value>0.003</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="PITCH">
|
||||
|
||||
<function name="aero/moment/Pitch_alpha">
|
||||
<description>Pitch moment due to alpha</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/cbarw-ft</property>
|
||||
<property>aero/alpha-rad</property>
|
||||
<value>-0.6</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Pitch_elevator">
|
||||
<description>Pitch moment due to elevator</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/cbarw-ft</property>
|
||||
<property>fcs/elevator-pos-rad</property>
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<tableData>
|
||||
0.0 -1.900
|
||||
2.0 -0.900
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Pitch_damp">
|
||||
<description>Pitch moment due to pitch rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/cbarw-ft</property>
|
||||
<property>aero/ci2vel</property>
|
||||
<property>velocities/q-aero-rad_sec</property>
|
||||
<value>-140</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Pitch_alphadot">
|
||||
<description>Pitch moment due to alpha rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/cbarw-ft</property>
|
||||
<property>aero/ci2vel</property>
|
||||
<property>aero/alphadot-rad_sec</property>
|
||||
<value>-1</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="YAW">
|
||||
|
||||
<function name="aero/moment/Yaw_beta">
|
||||
<description>Yaw moment due to beta</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/beta-rad</property>
|
||||
<value>0.12</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Yaw_damp">
|
||||
<description>Yaw moment due to yaw rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/bi2vel</property>
|
||||
<property>velocities/r-aero-rad_sec</property>
|
||||
<value>-0.2</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Yaw_rudder">
|
||||
<description>Yaw moment due to rudder</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>fcs/rudder-pos-rad</property>
|
||||
<value>-0.2</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Yaw_aileron">
|
||||
<description>Adverse yaw</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>fcs/left-aileron-pos-rad</property>
|
||||
<value>0</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
</aerodynamics>
|
||||
|
|
@ -1,5 +1,8 @@
|
|||
<?xml version="1.0" encoding="UTF-8"?>
|
||||
|
||||
<!-- A3XX CFM56 FADEC -->
|
||||
<!-- Joshua Davidson -->
|
||||
|
||||
<PropertyList>
|
||||
|
||||
<filter>
|
||||
|
|
@ -436,7 +439,7 @@
|
|||
</equals>
|
||||
<greater-than>
|
||||
<property>/engines/engine[0]/n1</property>
|
||||
<value>23</value>
|
||||
<value>22</value>
|
||||
</greater-than>
|
||||
</and>
|
||||
</condition>
|
||||
|
|
@ -469,7 +472,7 @@
|
|||
</equals>
|
||||
<greater-than>
|
||||
<property>/engines/engine[1]/n1</property>
|
||||
<value>23</value>
|
||||
<value>22</value>
|
||||
</greater-than>
|
||||
</and>
|
||||
</condition>
|
||||
|
|
|
|||
|
|
@ -1,5 +1,8 @@
|
|||
<?xml version="1.0" encoding="UTF-8"?>
|
||||
|
||||
<!-- A3XX IAE V2500 FADEC -->
|
||||
<!-- Joshua Davidson -->
|
||||
|
||||
<PropertyList>
|
||||
|
||||
<filter>
|
||||
|
|
@ -702,7 +705,7 @@
|
|||
</equals>
|
||||
<greater-than>
|
||||
<property>/engines/engine[0]/n1</property>
|
||||
<value>23</value>
|
||||
<value>22</value>
|
||||
</greater-than>
|
||||
</and>
|
||||
</condition>
|
||||
|
|
@ -735,7 +738,7 @@
|
|||
</equals>
|
||||
<greater-than>
|
||||
<property>/engines/engine[1]/n1</property>
|
||||
<value>23</value>
|
||||
<value>22</value>
|
||||
</greater-than>
|
||||
</and>
|
||||
</condition>
|
||||
|
|
@ -755,4 +758,4 @@
|
|||
<output>/engines/engine[1]/egt-actual</output>
|
||||
</filter>
|
||||
|
||||
</PropertyList>
|
||||
</PropertyList>
|
||||
Reference in a new issue