539 lines
14 KiB
XML
539 lines
14 KiB
XML
<!-- Airbus A320 Aerodynamics -->
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<!-- Joshua Davidson (it0uchpods) -->
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<!--
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##############################################
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# Copyright (c) Joshua Davidson (it0uchpods) #
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##############################################
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-->
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<aerodynamics>
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<property value="0.0">ice/wing</property>
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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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-1.57 -1.4000
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-1.22 -1.3512
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-1.05 -1.2426
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-0.88 -1.1575
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-0.64 -1.0312
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-0.25 -0.9379
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0.00 0.1494
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0.25 1.6072
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0.60 1.0305
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0.88 0.6415
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1.05 0.2294
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1.22 0.0544
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1.57 0.0000
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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_pitch_rate">
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<description>Lift 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>velocities/q-aero-rad_sec</property>
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<property>aero/ci2vel</property>
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<value>8.5404</value>
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</product>
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</function>
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<function name="aero/force/Lift_alpha_rate">
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<description>Lift 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>aero/alphadot-rad_sec</property>
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<property>aero/ci2vel</property>
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<value>2.9706</value>
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</product>
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</function>
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<function name="aero/force/Lift_pitch_control">
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<description>Lift due to pitch control 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/pitch-pos-geared</property>
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<value>0.2395</value>
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</product>
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</function>
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<function name="aero/force/Lift_pitch_trim_control">
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<description>Lift due to pitch trim control 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/pitch-trim-pos-geared</property>
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<value>0.2395</value>
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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 0.0000
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0.290 0.0648
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0.596 0.1017
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0.645 0.2404
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1.000 0.3066
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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_slat">
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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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<table>
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<independentVar lookup="row">fcs/slat-pos-norm</independentVar>
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<tableData>
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0.000 0.0000
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0.666 0.1734
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0.814 0.2509
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1.000 0.3113
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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_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>-0.1</value>
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</product>
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</function>
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<function name="aero/coefficient/CLicew">
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<description>Lift_decrease_due_to_ice_on_wing</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>ice/wing</independentVar>
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<tableData>
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0.0 0.0
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0.5 -0.1
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1.0 -0.3
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2.0 -1.5
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</tableData>
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</table>
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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_minimum">
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<description>Minimum 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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<value>0.0125</value>
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</product>
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</function>
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<function name="aero/force/Drag_alpha">
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<description>Drag 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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-1.57 1.3083
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-0.20 0.0331
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0.00 0.0000
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0.20 0.0331
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1.57 1.3083
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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>0.0384</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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0.20 0.000
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0.79 0.002
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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_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 1.23
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-0.26 0.05
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0.00 0.00
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0.26 0.05
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1.57 1.23
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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_pitch_control">
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<description>Drag due to pitch control 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/pitch-pos-geared</property></abs>
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<value>0.02</value>
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</product>
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</function>
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<function name="aero/force/Drag_pitch_trim_control">
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<description>Drag due to pitch trim control 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/pitch-trim-pos-geared</property></abs>
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<value>0.02</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>0.0175</value>
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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>0.00125</value>
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</product>
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</function>
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<function name="aero/force/Drag_slat">
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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/slat-pos-deg</property>
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<value>0.00125</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 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>0.0275</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>-0.8887</value>
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</product>
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</function>
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<function name="aero/force/Side_roll_rate">
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<description>Side force 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>aero/bi2vel</property>
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<property>velocities/p-aero-rad_sec</property>
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<table>
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<independentVar lookup="row">aero/Re</independentVar>
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<tableData>
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25661346 0.2466
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28227480 0.0178
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38492020 0.0079
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51187312 0.0045
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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/Side_yaw_rate">
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<description>Side force 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>aero/bi2vel</property>
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<property>velocities/r-aero-rad_sec</property>
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<value>0.8709</value>
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</product>
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</function>
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<function name="aero/force/Side_rudder">
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<description>Side force 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>fcs/rudder-pos-rad</property>
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<value>0.2653</value>
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</product>
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</function>
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<function name="aero/force/Drag_wingice">
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<description>Drag_due_to_ice_on_wing</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>ice/wing</independentVar>
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<tableData>
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0.0 0.000
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0.5 0.004
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1.0 0.010
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2.0 0.100
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</tableData>
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</table>
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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>-0.47</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>0.2</value>
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</product>
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</function>
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<function name="aero/moment/Roll_control">
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<description>Roll moment due to roll control</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/roll-pos-rad</property>
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<value>0.11</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>0.01</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>-0.7918</value>
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</product>
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</function>
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<function name="aero/moment/Pitch_control">
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<description>Pitch moment due to pitch control</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/pitch-pos-geared</property>
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<value>-1.825</value>
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</product>
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</function>
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<function name="aero/moment/Pitch_trim_control">
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<description>Pitch moment due to pitch trim control</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/pitch-trim-pos-geared</property>
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<value>-3.045</value>
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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>-37.4</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>-1.1356</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>0.1292</value>
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</product>
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</function>
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<function name="aero/moment/Yaw_roll_rate">
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<description>Yaw 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/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_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>-0.1</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>
|
|
<property>metrics/Sw-sqft</property>
|
|
<property>metrics/bw-ft</property>
|
|
<property>fcs/rudder-pos-rad</property>
|
|
<value>-0.053</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/roll-pos-rad</property>
|
|
<value>0</value>
|
|
</product>
|
|
</function>
|
|
|
|
</axis>
|
|
|
|
</aerodynamics>
|