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A32X: Rewrite Drag Axis, Fix NEOs using wrong vstab/hstab

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This commit is contained in:
Joshua Davidson 2017-06-16 17:35:23 -04:00
parent 596e038bfd
commit d182b21b61
5 changed files with 25 additions and 28 deletions
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4
Models/A320neo-CFM.xml
View file

@ -79,7 +79,7 @@
<model>
<name>Horizontal Stabilizer</name>
<path>Aircraft/A320Family/Models/Fuselages/A320/hstab.xml</path>
<path>Aircraft/A320Family/Models/Fuselages/A320neo/hstab.xml</path>
<offsets>
<x-m>34.1512207</x-m>
<pitch-deg>0.0</pitch-deg>
@ -88,7 +88,7 @@
<model>
<name>Vertical Stabilizer</name>
<path>Aircraft/A320Family/Models/Fuselages/A320/vstab.xml</path>
<path>Aircraft/A320Family/Models/Fuselages/A320neo/vstab.xml</path>
<offsets>
<x-m>32.2535728</x-m>
</offsets>

4
Models/A321neo-CFM.xml
View file

@ -78,7 +78,7 @@
<model>
<name>Horizontal Stabilizer</name>
<path>Aircraft/A320Family/Models/Fuselages/A321/hstab.xml</path>
<path>Aircraft/A320Family/Models/Fuselages/A321neo/hstab.xml</path>
<offsets>
<x-m>36.8212207</x-m>
<pitch-deg>0.0</pitch-deg>
@ -87,7 +87,7 @@
<model>
<name>Vertical Stabilizer</name>
<path>Aircraft/A320Family/Models/Fuselages/A321/vstab.xml</path>
<path>Aircraft/A320Family/Models/Fuselages/A321neo/vstab.xml</path>
<offsets>
<x-m>34.9235728</x-m>
</offsets>

15
Systems/a319-aerodynamics.xml
View file

@ -82,11 +82,11 @@
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<tableData>
-1.57 1.260
-0.26 0.018
-1.57 1.275
-0.26 0.025
0.00 0.008
0.26 0.017
1.57 1.320
0.26 0.019
1.57 1.322
</tableData>
</table>
</product>
@ -111,8 +111,7 @@
<independentVar lookup="row">velocities/mach</independentVar>
<tableData>
0.00 0.000
0.79 0.000
1.10 0.023
1.10 0.018
1.80 0.015
</tableData>
</table>
@ -125,7 +124,7 @@
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/flap-pos-deg</property>
<value> 0.00080 </value>
<value> 0.00110 </value>
</product>
</function>
@ -155,7 +154,7 @@
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/speedbrake-pos-norm</property>
<value>0.035</value>
<value>0.025</value>
</product>
</function>

15
Systems/a320-aerodynamics.xml
View file

@ -82,11 +82,11 @@
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<tableData>
-1.57 1.260
-0.26 0.018
-1.57 1.275
-0.26 0.025
0.00 0.008
0.26 0.017
1.57 1.320
0.26 0.019
1.57 1.322
</tableData>
</table>
</product>
@ -111,8 +111,7 @@
<independentVar lookup="row">velocities/mach</independentVar>
<tableData>
0.00 0.000
0.79 0.000
1.10 0.023
1.10 0.018
1.80 0.015
</tableData>
</table>
@ -125,7 +124,7 @@
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/flap-pos-deg</property>
<value> 0.00080 </value>
<value> 0.00110 </value>
</product>
</function>
@ -155,7 +154,7 @@
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/speedbrake-pos-norm</property>
<value>0.035</value>
<value>0.025</value>
</product>
</function>

15
Systems/a321-aerodynamics.xml
View file

@ -82,11 +82,11 @@
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<tableData>
-1.57 1.260
-0.26 0.018
-1.57 1.275
-0.26 0.025
0.00 0.008
0.26 0.017
1.57 1.320
0.26 0.019
1.57 1.322
</tableData>
</table>
</product>
@ -111,8 +111,7 @@
<independentVar lookup="row">velocities/mach</independentVar>
<tableData>
0.00 0.000
0.79 0.000
1.10 0.023
1.10 0.018
1.80 0.015
</tableData>
</table>
@ -125,7 +124,7 @@
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/flap-pos-deg</property>
<value> 0.00080 </value>
<value> 0.00110 </value>
</product>
</function>
@ -155,7 +154,7 @@
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/speedbrake-pos-norm</property>
<value>0.035</value>
<value>0.025</value>
</product>
</function>