A32X: FDM Aerodynamics rework, should be okay, needs testing
This commit is contained in:
Joshua Davidson
parent
9802fab6c0
commit
10c98be630
6 changed files with 264 additions and 169 deletions
|
|
@ -19,9 +19,9 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
|
|||
|
||||
<metrics>
|
||||
<wingarea unit="FT2"> 1319.79 </wingarea>
|
||||
<wingspan unit="FT" > 111.26 </wingspan>
|
||||
<wingspan unit="FT" > 117.26 </wingspan>
|
||||
<wing_incidence > 1.03 </wing_incidence>
|
||||
<chord unit="FT" > 13.76 </chord>
|
||||
<chord unit="FT" > 20.76 </chord>
|
||||
<htailarea unit="FT2"> 334.24 </htailarea>
|
||||
<htailarm unit="FT" > 57.88 </htailarm>
|
||||
<vtailarea unit="FT2"> 248.79 </vtailarea>
|
||||
|
|
|
|||
|
|
@ -19,9 +19,9 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
|
|||
|
||||
<metrics>
|
||||
<wingarea unit="FT2"> 1319.79 </wingarea>
|
||||
<wingspan unit="FT" > 111.26 </wingspan>
|
||||
<wingspan unit="FT" > 117.26 </wingspan>
|
||||
<wing_incidence > 1.03 </wing_incidence>
|
||||
<chord unit="FT" > 13.76 </chord>
|
||||
<chord unit="FT" > 20.76 </chord>
|
||||
<htailarea unit="FT2"> 334.24 </htailarea>
|
||||
<htailarm unit="FT" > 57.88 </htailarm>
|
||||
<vtailarea unit="FT2"> 248.79 </vtailarea>
|
||||
|
|
|
|||
|
|
@ -19,9 +19,9 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
|
|||
|
||||
<metrics>
|
||||
<wingarea unit="FT2"> 1319.79 </wingarea>
|
||||
<wingspan unit="FT" > 111.26 </wingspan>
|
||||
<wingspan unit="FT" > 117.26 </wingspan>
|
||||
<wing_incidence > 1.03 </wing_incidence>
|
||||
<chord unit="FT" > 13.76 </chord>
|
||||
<chord unit="FT" > 20.76 </chord>
|
||||
<htailarea unit="FT2"> 334.24 </htailarea>
|
||||
<htailarm unit="FT" > 57.88 </htailarm>
|
||||
<vtailarea unit="FT2"> 248.79 </vtailarea>
|
||||
|
|
|
|||
|
|
@ -19,9 +19,9 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
|
|||
|
||||
<metrics>
|
||||
<wingarea unit="FT2"> 1319.79 </wingarea>
|
||||
<wingspan unit="FT" > 111.26 </wingspan>
|
||||
<wingspan unit="FT" > 117.26 </wingspan>
|
||||
<wing_incidence > 1.03 </wing_incidence>
|
||||
<chord unit="FT" > 13.76 </chord>
|
||||
<chord unit="FT" > 20.76 </chord>
|
||||
<htailarea unit="FT2"> 334.24 </htailarea>
|
||||
<htailarm unit="FT" > 57.88 </htailarm>
|
||||
<vtailarea unit="FT2"> 248.79 </vtailarea>
|
||||
|
|
|
|||
|
|
@ -19,9 +19,9 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
|
|||
|
||||
<metrics>
|
||||
<wingarea unit="FT2"> 1319.79 </wingarea>
|
||||
<wingspan unit="FT" > 111.26 </wingspan>
|
||||
<wingspan unit="FT" > 117.26 </wingspan>
|
||||
<wing_incidence > 1.03 </wing_incidence>
|
||||
<chord unit="FT" > 13.76 </chord>
|
||||
<chord unit="FT" > 20.76 </chord>
|
||||
<htailarea unit="FT2"> 334.24 </htailarea>
|
||||
<htailarm unit="FT" > 57.88 </htailarm>
|
||||
<vtailarea unit="FT2"> 248.79 </vtailarea>
|
||||
|
|
|
|||
|
|
@ -1,4 +1,4 @@
|
|||
<!-- A3XX Aerodynamics -->
|
||||
<!-- Airbus A320 Aerodynamics -->
|
||||
<!-- Joshua Davidson (it0uchpods) -->
|
||||
|
||||
<!--
|
||||
|
|
@ -21,16 +21,56 @@
|
|||
<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
|
||||
-1.57 -1.4000
|
||||
-1.22 -1.3512
|
||||
-1.05 -1.2426
|
||||
-0.88 -1.1575
|
||||
-0.64 -1.0312
|
||||
-0.25 -0.9379
|
||||
0.00 0.1494
|
||||
0.20 1.6072
|
||||
0.60 0.9705
|
||||
0.88 0.4415
|
||||
1.05 0.1294
|
||||
1.22 0.0544
|
||||
1.57 0.0000
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Lift_pitch_rate">
|
||||
<description>Lift due to pitch rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>velocities/q-aero-rad_sec</property>
|
||||
<property>aero/ci2vel</property>
|
||||
<value>8.5404</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Lift_alpha_rate">
|
||||
<description>Lift due to alpha rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>aero/alphadot-rad_sec</property>
|
||||
<property>aero/ci2vel</property>
|
||||
<value>2.9706</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/pitch-pos-geared</property>
|
||||
<value>0.4791</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Lift_flap">
|
||||
<description>Delta Lift due to flaps</description>
|
||||
<product>
|
||||
|
|
@ -39,23 +79,30 @@
|
|||
<table>
|
||||
<independentVar lookup="row">fcs/flap-pos-norm</independentVar>
|
||||
<tableData>
|
||||
0.000 0.00000
|
||||
0.290 0.00250
|
||||
0.596 0.00700
|
||||
0.645 0.01400
|
||||
1.000 0.01800
|
||||
0.000 0.0000
|
||||
0.290 0.0648
|
||||
0.596 0.1017
|
||||
0.645 0.2404
|
||||
1.000 0.2866
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Lift_slats">
|
||||
<function name="aero/force/Lift_slat">
|
||||
<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>
|
||||
<table>
|
||||
<independentVar lookup="row">fcs/slat-pos-norm</independentVar>
|
||||
<tableData>
|
||||
0.000 0.0000
|
||||
0.666 0.1734
|
||||
0.814 0.2509
|
||||
1.000 0.3113
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
|
|
@ -65,17 +112,7 @@
|
|||
<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_pitch_control">
|
||||
<description>Lift due to pitch control deflection</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/pitch-pos-geared</property>
|
||||
<value>0.04</value>
|
||||
<value>-0.1</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
|
|
@ -87,7 +124,7 @@
|
|||
<table>
|
||||
<independentVar>ice/wing</independentVar>
|
||||
<tableData>
|
||||
0.0 0
|
||||
0.0 0.0
|
||||
0.5 -0.1
|
||||
1.0 -0.3
|
||||
2.0 -1.5
|
||||
|
|
@ -95,23 +132,33 @@
|
|||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="DRAG">
|
||||
|
||||
<function name="aero/force/Drag_basic">
|
||||
<description>Drag at zero lift</description>
|
||||
<function name="aero/force/Drag_minimum">
|
||||
<description>Minimum drag</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<value>0.0125</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_alpha">
|
||||
<description>Drag due to alpha</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">aero/alpha-rad</independentVar>
|
||||
<tableData>
|
||||
-1.57 1.275
|
||||
-0.26 0.025
|
||||
0.00 0.008
|
||||
0.26 0.025
|
||||
1.57 1.322
|
||||
-1.57 1.2083
|
||||
-0.20 0.0231
|
||||
0.00 0.0000
|
||||
0.20 0.0231
|
||||
1.57 1.2083
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
|
|
@ -123,7 +170,7 @@
|
|||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>aero/cl-squared</property>
|
||||
<value>0.036</value>
|
||||
<value>0.0377</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
|
|
@ -136,53 +183,14 @@
|
|||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<tableData>
|
||||
0.00 0.000
|
||||
1.10 0.017
|
||||
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> 0.00120 </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/slat-pos-deg</property>
|
||||
<value> 0.00100 </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>0.025</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_beta">
|
||||
<description>Drag due to sideslip</description>
|
||||
<product>
|
||||
|
|
@ -191,33 +199,63 @@
|
|||
<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
|
||||
-1.57 1.23
|
||||
-0.26 0.05
|
||||
0.00 0.00
|
||||
0.26 0.05
|
||||
1.57 1.23
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_pitch_control">
|
||||
<description>Drag due to pitch control deflection</description>
|
||||
<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/pitch-pos-rad</property></abs>
|
||||
<value>0.07</value>
|
||||
<abs><property>fcs/pitch-pos-geared</property></abs>
|
||||
<value>0.04</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_pitch_trim_control">
|
||||
<description>Drag due to pitch trim control deflection</description>
|
||||
<function name="aero/force/Drag_gear">
|
||||
<description>Drag due to gear</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<abs><property>fcs/pitch-trim-pos-rad</property></abs>
|
||||
<value>0.07</value>
|
||||
<property>gear/gear-pos-norm</property>
|
||||
<value>0.0175</value>
|
||||
</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>0.00125</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_slat">
|
||||
<description>Drag due to slats</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/slat-pos-deg</property>
|
||||
<value>0.00125</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_speedbrake">
|
||||
<description>Drag due to speedbrake</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/speedbrake-pos-norm</property>
|
||||
<value>0.0275</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
|
|
@ -231,7 +269,47 @@
|
|||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>aero/beta-rad</property>
|
||||
<value>-1</value>
|
||||
<value>-0.8887</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Side_roll_rate">
|
||||
<description>Side force due to roll rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>aero/bi2vel</property>
|
||||
<property>velocities/p-aero-rad_sec</property>
|
||||
<table>
|
||||
<independentVar lookup="row">aero/Re</independentVar>
|
||||
<tableData>
|
||||
25661346 0.2466
|
||||
28227480 0.0178
|
||||
38492020 0.0079
|
||||
51187312 0.0045
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Side_yaw_rate">
|
||||
<description>Side force due to yaw rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>aero/bi2vel</property>
|
||||
<property>velocities/r-aero-rad_sec</property>
|
||||
<value>0.8709</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Side_rudder">
|
||||
<description>Side force due to rudder</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/rudder-pos-rad</property>
|
||||
<value>0.2653</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
|
|
@ -243,7 +321,7 @@
|
|||
<table>
|
||||
<independentVar>ice/wing</independentVar>
|
||||
<tableData>
|
||||
0.0 0
|
||||
0.0 0.000
|
||||
0.5 0.004
|
||||
1.0 0.010
|
||||
2.0 0.100
|
||||
|
|
@ -263,7 +341,15 @@
|
|||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/beta-rad</property>
|
||||
<value>-0.05</value>
|
||||
<table>
|
||||
<independentVar lookup="row">aero/alpha-rad</independentVar>
|
||||
<independentVar lookup="column">aero/Re</independentVar>
|
||||
<tableData>
|
||||
25661346 28227480 38492020 51187312
|
||||
-0.0349 -0.1815 -0.0991 -0.0970 -0.1010
|
||||
0.3491 -1.6241 -0.3352 -0.3924 -0.6078
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
|
|
@ -287,7 +373,15 @@
|
|||
<property>metrics/bw-ft</property>
|
||||
<property>aero/bi2vel</property>
|
||||
<property>velocities/r-aero-rad_sec</property>
|
||||
<value>0.005</value>
|
||||
<table>
|
||||
<independentVar lookup="row">aero/alpha-rad</independentVar>
|
||||
<independentVar lookup="column">aero/Re</independentVar>
|
||||
<tableData>
|
||||
25661346 28227480 38492020 51187312
|
||||
-0.0349 0.0028 0.0028 0.0028 0.0028
|
||||
0.3491 2.2829 0.2608 0.2608 0.2608
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
|
|
@ -324,7 +418,7 @@
|
|||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/cbarw-ft</property>
|
||||
<property>aero/alpha-rad</property>
|
||||
<value>-0.6</value>
|
||||
<value>-0.7918</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
|
|
@ -370,7 +464,7 @@
|
|||
<property>metrics/cbarw-ft</property>
|
||||
<property>aero/ci2vel</property>
|
||||
<property>aero/alphadot-rad_sec</property>
|
||||
<value>-1</value>
|
||||
<value>-1.1356</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
|
|
@ -385,12 +479,12 @@
|
|||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/beta-rad</property>
|
||||
<value>0.12</value>
|
||||
<value>0.1292</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Yaw_damp">
|
||||
<description>Yaw moment due to yaw rate</description>
|
||||
<function name="aero/moment/Yaw_roll_rate">
|
||||
<description>Yaw moment due to roll rate</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
|
|
@ -418,10 +512,11 @@
|
|||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>fcs/left-aileron-pos-rad</property>
|
||||
<property>fcs/roll-pos-rad</property>
|
||||
<value>0</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
</aerodynamics>
|
||||
|
|
|
|||
Reference in a new issue