670 lines
19 KiB
XML
670 lines
19 KiB
XML
<!-- Airbus A320 Aerodynamics -->
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<!-- Copyright (c) 2020 Josh Davidson (Octal450) -->
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<aerodynamics>
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<property value="0.0">ice/wingL</property>
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<property value="0.0">ice/wingR</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 1.6272
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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>6.9404</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>1.9706</value>
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</product>
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</function>
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<function name="aero/force/Lift_left_elevator">
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<description>Lift due to left 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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<toradians><property>hydraulics/elevator-l/final-deg</property></toradians>
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<value>0.0936445</value>
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</product>
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</function>
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<function name="aero/force/Lift_right_elevator">
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<description>Lift due to right 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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<toradians><property>hydraulics/elevator-r/final-deg</property></toradians>
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<value>0.0936445</value>
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</product>
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</function>
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<function name="aero/force/Lift_elevator_trim_control">
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<description>Lift due to elevator 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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<toradians><property>hydraulics/elevator-trim/final-deg</property></toradians>
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<value>0.0118082</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 0.0948
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0.596 0.1617
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0.645 0.2704
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1.000 0.3466
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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 0.2334
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0.814 0.2809
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1.000 0.3323
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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_left_spoiler">
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<description>Delta Lift due to left spoiler</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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<toradians><property>fcs/spoiler-left-deg</property></toradians>
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<value>-0.0523599</value>
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</product>
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</function>
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<function name="aero/force/Lift_right_spoiler">
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<description>Delta Lift due to right spoiler</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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<toradians><property>fcs/spoiler-right-deg</property></toradians>
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<value>-0.0523599</value>
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</product>
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</function>
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<function name="aero/coefficient/CLicewl">
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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/wingL</independentVar>
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<tableData>
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0.0 0.00
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0.5 -0.05
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1.0 -0.15
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2.0 -1.25
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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/coefficient/CLicewr">
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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/wingR</independentVar>
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<tableData>
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0.0 0.0
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0.5 -0.05
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1.0 -0.15
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2.0 -1.25
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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 0.0301
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0.00 0.0000
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0.20 0.0301
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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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0.82 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_left_elevator">
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<description>Drag due to left 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><toradians><property>hydraulics/elevator-l/final-deg</property></toradians></abs>
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<value>0.00782</value>
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</product>
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</function>
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<function name="aero/force/Drag_right_elevator">
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<description>Drag due to right 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><toradians><property>hydraulics/elevator-r/final-deg</property></toradians></abs>
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<value>0.00782</value>
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</product>
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</function>
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<function name="aero/force/Drag_elevator_trim_control">
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<description>Drag due to elevator 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><toradians><property>hydraulics/elevator-trim/final-deg</property></toradians></abs>
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<value>0.01564</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_left_aileron">
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<description>Drag due to left 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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<abs><toradians><property>hydraulics/aileron-l/final-deg</property></toradians></abs>
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<value>0.00811826141696</value>
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</product>
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</function>
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<function name="aero/force/Drag_left_spoiler">
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<description>Drag due to left spoiler</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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<toradians><property>fcs/spoiler-left-deg</property></toradians>
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<value>0.025369566928</value>
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</product>
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</function>
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<function name="aero/force/Drag_right_spoiler">
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<description>Drag due to right spoiler</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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<toradians><property>fcs/spoiler-right-deg</property></toradians>
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<value>0.025369566928</value>
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</product>
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</function>
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<function name="aero/force/Drag_right_aileron">
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<description>Drag due to right 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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<abs><toradians><property>hydraulics/aileron-r/final-deg</property></toradians></abs>
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<value>0.00811826141696</value>
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</product>
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</function>
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<function name="aero/force/Drag_wingicel">
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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/wingL</independentVar>
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<tableData>
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0.0 0.000
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0.5 0.002
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1.0 0.005
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2.0 0.050
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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_wingicer">
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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/wingR</independentVar>
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<tableData>
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0.0 0.000
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0.5 0.002
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1.0 0.005
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2.0 0.050
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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_landing_light_left">
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<description>Drag due to left landing light</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>rubbish/landL</property>
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<value>0.0016</value>
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</product>
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</function>
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<function name="aero/force/Drag_landing_light_right">
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<description>Drag due to right landing light</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>rubbish/landR</property>
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<value>0.0016</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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<toradians><property>hydraulics/rudder/final-deg</property></toradians>
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<value>-0.2653</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>-0.47</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>0.1</value>
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</product>
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</function>
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<function name="aero/moment/Roll_left_aileron">
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<description>Roll moment due to left aileron</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>
|
|
<toradians><property>hydraulics/aileron-l/final-deg</property></toradians>
|
|
<value>0.044</value>
|
|
</product>
|
|
</function>
|
|
|
|
<function name="aero/moment/Roll_right_aileron">
|
|
<description>Roll moment due to right aileron</description>
|
|
<product>
|
|
<property>aero/qbar-psf</property>
|
|
<property>metrics/Sw-sqft</property>
|
|
<property>metrics/bw-ft</property>
|
|
<toradians><property>hydraulics/aileron-r/final-deg</property></toradians>
|
|
<value>-0.044</value>
|
|
</product>
|
|
</function>
|
|
|
|
<function name="aero/moment/Roll_left_spoiler">
|
|
<description>Roll moment due to left spoiler</description>
|
|
<product>
|
|
<property>aero/qbar-psf</property>
|
|
<property>metrics/Sw-sqft</property>
|
|
<property>metrics/bw-ft</property>
|
|
<toradians><property>fcs/spoiler-left-deg</property></toradians>
|
|
<value>-0.033</value>
|
|
</product>
|
|
</function>
|
|
|
|
<function name="aero/moment/Roll_right_spoiler">
|
|
<description>Roll moment due to right spoiler</description>
|
|
<product>
|
|
<property>aero/qbar-psf</property>
|
|
<property>metrics/Sw-sqft</property>
|
|
<property>metrics/bw-ft</property>
|
|
<toradians><property>fcs/spoiler-right-deg</property></toradians>
|
|
<value>0.033</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>
|
|
<toradians><property>hydraulics/rudder/final-deg</property></toradians>
|
|
<value>0.01</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>-0.5918</value>
|
|
</product>
|
|
</function>
|
|
|
|
<function name="aero/moment/Pitch_left_elevator">
|
|
<description>Pitch moment due to left elevator</description>
|
|
<product>
|
|
<property>aero/qbar-psf</property>
|
|
<property>metrics/Sw-sqft</property>
|
|
<property>metrics/cbarw-ft</property>
|
|
<toradians><property>hydraulics/elevator-l/final-deg</property></toradians>
|
|
<value>-0.557175</value>
|
|
</product>
|
|
</function>
|
|
|
|
<function name="aero/moment/Pitch_right_elevator">
|
|
<description>Pitch moment due to right elevator</description>
|
|
<product>
|
|
<property>aero/qbar-psf</property>
|
|
<property>metrics/Sw-sqft</property>
|
|
<property>metrics/cbarw-ft</property>
|
|
<toradians><property>hydraulics/elevator-r/final-deg</property></toradians>
|
|
<value>-0.557175</value>
|
|
</product>
|
|
</function>
|
|
|
|
<function name="aero/moment/Pitch_elevator_trim">
|
|
<description>Pitch moment due to elevator trim control</description>
|
|
<product>
|
|
<property>aero/qbar-psf</property>
|
|
<property>metrics/Sw-sqft</property>
|
|
<property>metrics/cbarw-ft</property>
|
|
<toradians><property>hydraulics/elevator-trim/final-deg</property></toradians>
|
|
<value>-2.22479</value>
|
|
</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>-37.4</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>-1.0356</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>0.1292</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>-0.3</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>
|
|
<toradians><property>hydraulics/rudder/final-deg</property></toradians>
|
|
<value>0.067</value>
|
|
</product>
|
|
</function>
|
|
|
|
</axis>
|
|
|
|
</aerodynamics>
|