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Aerodynamicschannel written new, old one was a chaos.

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This commit is contained in:
JWocky 2016-11-08 16:11:39 -06:00
parent 34c3f1024b
commit d2f2b26bb9
2 changed files with 398 additions and 746 deletions
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152
A320-200-IAE (changed CG).xml → A320-200-IAE (before rewriting aerodynamics channel).xml
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@ -30,7 +30,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
<z> -25.2091 </z> <z> -25.2091 </z>
</location --> </location -->
<location name="AERORP" unit="IN"> <location name="AERORP" unit="IN">
<x> 650.00 </x> <x> 680.00 </x>
<y> 0 </y> <y> 0 </y>
<z> 0.00 </z> <z> 0.00 </z>
</location> </location>
@ -75,8 +75,8 @@ YAW MOI_________3950000______23089847_______24848934
<iyz unit="SLUG*FT2"> 0 </iyz> <iyz unit="SLUG*FT2"> 0 </iyz>
<emptywt unit="LBS">80431</emptywt> <!-- #ref-1 page 67, WV016. 90927lbs - 5248x2 (engines)=80431lbs--> <emptywt unit="LBS">80431</emptywt> <!-- #ref-1 page 67, WV016. 90927lbs - 5248x2 (engines)=80431lbs-->
<!-- #### PB: That makes no sense, the wohle aircraft is 1479.1339 inches long. 650inches eqauls to about 43.95% MAC with the Airbus limits according to the AMM between 45% and 49% <!-- #### PB: That makes no sense, the whole aircraft is 1479.1339 inches long. 650inches eqauls to about 43.95% MAC with the Airbus limits according to the AMM between 45% and 49%
Also: The z-axis is -41.73 unches under the zero line of the plane while the pressure point is only -25,91 under the same line and slightly ahead, that causes the plane to behave quite unstable Also: The z-axis is -41.73 inches under the zero line of the plane while the pressure point is only -25,91 under the same line and slightly ahead, that causes the plane to behave quite unstable
--> -->
<!-- location name="CG" unit="IN"> <!-- location name="CG" unit="IN">
<! - -x> 642.122 </x- - > <! - -x> 642.122 </x- - >
@ -85,104 +85,82 @@ YAW MOI_________3950000______23089847_______24848934
<z> -41.7398 </z> <z> -41.7398 </z>
</location --> </location -->
<location name="CG" unit="IN"> <location name="CG" unit="IN">
<x> 650.00 </x> <x> 655.00 </x>
<y> 0 </y> <y> 0 </y>
<z> 0.00 </z> <z> 0.00 </z>
</location> </location>
<pointmass name="Crew"> <pointmass name="Cockpit Crew">
<weight unit="LBS">400</weight> <!-- MAX: 600lbs--> <weight unit="LBS">400</weight> <!-- MAX: 400lbs, two pilots-->
<location name="POINTMASS" unit="IN"> <location name="POINTMASS" unit="IN">
<x>200</x> <x>200</x>
<y>0</y> <y>0</y>
<z>0</z> <z>0</z>
</location> </location>
</pointmass> </pointmass>
<pointmass name="PAX"> <pointmass name="Cabin Crew">
<weight unit="LBS">19750</weight> <!-- MAX: 39500 lbs ** looks too heavy. maybe low it and give a long cilinder shape. need to do some maths--> <weight unit="LBS">600</weight> <!-- MAX: 1320lbs, up to six flight-attendants-->
<form shape="cylinder">
<radius unit="M"> 2.13 </radius>
<length unit="M"> 24.44 </length>
</form>
<location name="POINTMASS" unit="IN"> <location name="POINTMASS" unit="IN">
<x>705</x> <x>696</x>
<y>0</y> <y>0</y>
<z>0</z> <z>0</z>
</location> </location>
</pointmass> </pointmass>
<pointmass name="PAX 0A (60 seats)">
<!-- NEW Pointmasses Start Weights for good CG --> <weight unit="LBS">6600</weight> <!-- MAX: 13200lbs, 60 seats -->
<pointmass name="Fwd Cargo">
<weight unit="LBS">3750</weight> <!-- #REF-3 page 19, MAX 3402 kilograms = 7500.12616 lbs -->
<form shape="cylinder">
<radius unit="M"> 1.24 </radius>
<length unit="M"> 4.95 </length>
</form>
<location name="POINTMASS" unit="IN"> <location name="POINTMASS" unit="IN">
<!-- #REF-1 page 88+98, <x>450.1711</x>
x= (door form nose(8.16m))-(door with(1.816m)/2)+(Cargo compartment lenght(4.953m)/2)
x= 9.7285 meters = 383.011811 in
-->
<x>383.01</x>
<y>0</y> <y>0</y>
<z>-59.05</z> <!-- Aprox lower deck 1.5 meters = 59.0551181 in --> <z>0</z>
</location> </location>
</pointmass> </pointmass>
<pointmass name="PAX 0B (60 seats)">
<pointmass name="Aft Cargo"> <weight unit="LBS">6600</weight> <!-- MAX: 13200lbs, 60 seats -->
<weight unit="LBS">0</weight> <!-- #REF-3 page 19, MAX 4536 kilograms = 10000.1682 lbs -->
<form shape="cylinder">
<radius unit="M"> 1.24 </radius>
<length unit="M"> 6.6 </length>
</form>
<location name="POINTMASS" unit="IN"> <location name="POINTMASS" unit="IN">
<!-- #REF-1 page 88+98, <x>739.5669</x>
x= (door form nose(22.69m))-(door with(1.816m)/2)
x= 21.78200 meters = 857.559055 in
-->
<x>857.55</x>
<y>0</y> <y>0</y>
<z>-59.05</z> <!-- Aprox lower deck 1.5 meters = 59.0551181 in --> <z>0</z>
</location> </location>
</pointmass> </pointmass>
<pointmass name="Rear Bulk Cargo"> <pointmass name="PAX 0C (54 seats)">
<weight unit="LBS">0</weight> <!-- #REF-3 page 19, MAX 1497 kilograms = 3300.32006 lbs --> <weight unit="LBS">5940</weight> <!-- MAX: 11880lbs, 54 seats -->
<form shape="cylinder">
<radius unit="M"> 1.24 </radius>
<length unit="M"> 2 </length>
</form>
<location name="POINTMASS" unit="IN"> <location name="POINTMASS" unit="IN">
<!-- #REF-1 page 88+102, <x>1093.2729</x>
x= (door form nose(22.69m))+(door with(1.816m)/2)+( Dist. between rear doors(2.19))+(Aprox to compartment center (2m))
x= 27.78800 meters = 1 094.01575 in
-->
<x>1094</x>
<y>0</y> <y>0</y>
<z>-39.37</z> <!-- Aprox bulk lower deck 1 meter = 39.3700787 in --> <z>0</z>
</location> </location>
</pointmass> </pointmass>
<pointmass name="Engine1"> <pointmass name="Cargo Hold 1">
<weight unit="LBS">5248</weight> <weight unit="LBS">2000</weight> <!-- MAX: 7500.126lbs -->
<form shape="cylinder">
<radius unit="M"> 1.31 </radius>
<length unit="M"> 5 </length>
</form>
<location name="POINTMASS" unit="IN"> <location name="POINTMASS" unit="IN">
<x>589.735</x> <x>383.4792</x>
<y>-226.575</y> <y>0</y>
<z>-45.567</z> <z>-29.5</z> <!-- 1.5m and now half of it for the center point of the load -->
</location> </location>
</pointmass> </pointmass>
<pointmass name="Engine2"> <!-- Cargo Hold 2 doesn't exist, that is the center tank -->
<weight unit="LBS">5248</weight> <pointmass name="Cargo Hold 3">
<form shape="cylinder"> <weight unit="LBS">2000</weight> <!-- MAX: 5384.414lbs -->
<radius unit="M"> 1.31 </radius>
<length unit="M"> 5 </length>
</form>
<location name="POINTMASS" unit="IN"> <location name="POINTMASS" unit="IN">
<x>589.735</x> <x>849.1324</x>
<y>226.575</y> <y>0</y>
<z>-45.567</z> <z>-29.5</z>
</location>
</pointmass>
<pointmass name="Cargo Hold 4">
<weight unit="LBS">1500</weight> <!-- MAX: 4651.754lbs -->
<location name="POINTMASS" unit="IN">
<x>931.0653</x>
<y>0</y>
<z>-29.5</z>
</location>
</pointmass>
<pointmass name="Cargo Hold 5">
<weight unit="LBS">2000</weight> <!-- MAX: 3300.320lbs -->
<location name="POINTMASS" unit="IN">
<x>1068.2634</x>
<y>0</y>
<z>0</z> <!-- Cargo Hold #5 sits higher on the range of the cabin deck, it's only loadable with lifter -->
</location> </location>
</pointmass> </pointmass>
@ -430,6 +408,7 @@ YAW MOI_________3950000______23089847_______24848934
</ground_reactions> </ground_reactions>
<propulsion> <propulsion>
<engine file="v2527_a5"> <engine file="v2527_a5">
<location unit="IN"> <location unit="IN">
<x> 589.735 </x> <x> 589.735 </x>
@ -457,6 +436,7 @@ YAW MOI_________3950000______23089847_______24848934
</orient> </orient>
</thruster> </thruster>
</engine> </engine>
<engine file="v2527_a5"> <engine file="v2527_a5">
<location unit="IN"> <location unit="IN">
<x> 589.735 </x> <x> 589.735 </x>
@ -488,7 +468,7 @@ YAW MOI_________3950000______23089847_______24848934
<tank type="FUEL"> <!-- Left Tank (Wing tip Ventilation Surge) 0 --> <tank type="FUEL"> <!-- Left Tank (Wing tip Ventilation Surge) 0 -->
<location unit="IN"> <location unit="IN">
<x> 788.4322 </x> <x> 783.0709 </x>
<y> -574.4148 </y> <y> -574.4148 </y>
<z> 3.1080 </z> <z> 3.1080 </z>
</location> </location>
@ -501,11 +481,11 @@ YAW MOI_________3950000______23089847_______24848934
</tank> </tank>
<tank type="FUEL"> <!-- Left Tank (Outer) 1 --> <tank type="FUEL"> <!-- Left Tank (Outer) 1 -->
<location unit="IN"> <location unit="IN">
<x> 737.4190 </x> <x> 739.5669 </x>
<y> -457.4259 </y> <y> -457.4259 </y>
<z> -8.0898 </z> <z> -8.0898 </z>
</location> </location>
<capacity unit="LBS"> 1548.8 </capacity><!-- need review --> <capacity unit="LBS"> 1520.00 </capacity><!-- need review -->
<contents unit="LBS"> 154.88 </contents> <contents unit="LBS"> 154.88 </contents>
<standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes --> <standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
<priority>2</priority> <priority>2</priority>
@ -514,12 +494,12 @@ YAW MOI_________3950000______23089847_______24848934
</tank> </tank>
<tank type="FUEL"> <!-- Left Tank (Inner) 2 --> <tank type="FUEL"> <!-- Left Tank (Inner) 2 -->
<location unit="IN"> <location unit="IN">
<x> 630.6588 </x> <x> 652.5591 </x>
<y> -236.2992 </y> <y> -236.2992 </y>
<z> -33.9470 </z> <z> -33.9470 </z>
</location> </location>
<capacity unit="LBS"> 12186.9 </capacity><!-- need review --> <capacity unit="LBS"> 11982 </capacity><!-- need review -->
<contents unit="LBS"> 2437.38 </contents> <contents unit="LBS"> 11982 </contents>
<standpipe unit="LBS">31</standpipe><!-- minimun fuel on pipes --> <standpipe unit="LBS">31</standpipe><!-- minimun fuel on pipes -->
<priority>3</priority> <priority>3</priority>
<type>JET-A1</type> <type>JET-A1</type>
@ -527,12 +507,12 @@ YAW MOI_________3950000______23089847_______24848934
</tank> </tank>
<tank type="FUEL"> <!-- Center Tank 3 --> <tank type="FUEL"> <!-- Center Tank 3 -->
<location unit="IN"> <location unit="IN">
<x> 580.9955 </x> <x> 522.0473 </x>
<y> 0 </y> <y> 0 </y>
<z> -47.0 </z> <z> -47.0 </z>
</location> </location>
<capacity unit="LBS"> 14520 </capacity><!-- need review --> <capacity unit="LBS"> 14281 </capacity><!-- need review -->
<contents unit="LBS"> 0 </contents> <contents unit="LBS"> 7260 </contents>
<standpipe unit="LBS">43</standpipe><!-- minimun fuel on pipes --> <standpipe unit="LBS">43</standpipe><!-- minimun fuel on pipes -->
<priority>1</priority> <priority>1</priority>
<type>JET-A1</type> <type>JET-A1</type>
@ -540,24 +520,24 @@ YAW MOI_________3950000______23089847_______24848934
</tank> </tank>
<tank type="FUEL"> <!-- Right Tank (Inner) 4 --> <tank type="FUEL"> <!-- Right Tank (Inner) 4 -->
<location unit="IN"> <location unit="IN">
<x> 630.6588 </x> <x> 652.5591 </x>
<y> 236.2992 </y> <y> 236.2992 </y>
<z> -33.9470 </z> <z> -33.9470 </z>
</location> </location>
<capacity unit="LBS"> 12186.9 </capacity><!-- need review --> <capacity unit="LBS"> 11982 </capacity><!-- need review -->
<contents unit="LBS"> 2437.38 </contents> <contents unit="LBS"> 11982 </contents>
<standpipe unit="LBS">31</standpipe><!-- minimun fuel on pipes --> <standpipe unit="LBS">31</standpipe><!-- minimum fuel on pipes -->
<priority>3</priority> <priority>3</priority>
<type>JET-A1</type> <type>JET-A1</type>
<temperature>50</temperature> <temperature>50</temperature>
</tank> </tank>
<tank type="FUEL"> <!-- Right Tank (Outer) 5 --> <tank type="FUEL"> <!-- Right Tank (Outer) 5 -->
<location unit="IN"> <location unit="IN">
<x> 737.4190 </x> <x> 739.5669 </x>
<y> 457.4259 </y> <y> 457.4259 </y>
<z> -8.0898 </z> <z> -8.0898 </z>
</location> </location>
<capacity unit="LBS"> 1548.8 </capacity><!-- need review --> <capacity unit="LBS"> 1520 </capacity><!-- need review -->
<contents unit="LBS"> 154.88 </contents> <contents unit="LBS"> 154.88 </contents>
<standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes --> <standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
<priority>2</priority> <priority>2</priority>
@ -566,7 +546,7 @@ YAW MOI_________3950000______23089847_______24848934
</tank> </tank>
<tank type="FUEL"> <!-- Right Tank (Wing tip Ventilation Surge) 6 --> <tank type="FUEL"> <!-- Right Tank (Wing tip Ventilation Surge) 6 -->
<location unit="IN"> <location unit="IN">
<x> 788.4322 </x> <x> 783.0709 </x>
<y> 574.4148 </y> <y> 574.4148 </y>
<z> 3.1080 </z> <z> 3.1080 </z>
</location> </location>

968
A320-200-IAE.xml
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