Aerodynamicschannel written new, old one was a chaos.
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JWocky
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34c3f1024b
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d2f2b26bb9
2 changed files with 398 additions and 746 deletions
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@ -30,7 +30,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
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<z> -25.2091 </z>
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</location -->
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<location name="AERORP" unit="IN">
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<x> 650.00 </x>
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<x> 680.00 </x>
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<y> 0 </y>
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<z> 0.00 </z>
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</location>
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@ -75,8 +75,8 @@ YAW MOI_________3950000______23089847_______24848934
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<iyz unit="SLUG*FT2"> 0 </iyz>
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<emptywt unit="LBS">80431</emptywt> <!-- #ref-1 page 67, WV016. 90927lbs - 5248x2 (engines)=80431lbs-->
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<!-- #### 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%
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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
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<!-- #### 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%
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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
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-->
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<!-- location name="CG" unit="IN">
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<! - -x> 642.122 </x- - >
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@ -85,104 +85,82 @@ YAW MOI_________3950000______23089847_______24848934
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<z> -41.7398 </z>
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</location -->
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<location name="CG" unit="IN">
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<x> 650.00 </x>
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<x> 655.00 </x>
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<y> 0 </y>
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<z> 0.00 </z>
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</location>
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<pointmass name="Crew">
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<weight unit="LBS">400</weight> <!-- MAX: 600lbs-->
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<pointmass name="Cockpit Crew">
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<weight unit="LBS">400</weight> <!-- MAX: 400lbs, two pilots-->
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<location name="POINTMASS" unit="IN">
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<x>200</x>
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<y>0</y>
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<z>0</z>
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</location>
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</pointmass>
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<pointmass name="PAX">
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<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-->
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<form shape="cylinder">
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<radius unit="M"> 2.13 </radius>
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<length unit="M"> 24.44 </length>
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</form>
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<pointmass name="Cabin Crew">
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<weight unit="LBS">600</weight> <!-- MAX: 1320lbs, up to six flight-attendants-->
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<location name="POINTMASS" unit="IN">
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<x>705</x>
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<x>696</x>
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<y>0</y>
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<z>0</z>
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</location>
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</pointmass>
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<!-- NEW Pointmasses Start Weights for good CG -->
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<pointmass name="Fwd Cargo">
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<weight unit="LBS">3750</weight> <!-- #REF-3 page 19, MAX 3402 kilograms = 7500.12616 lbs -->
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<form shape="cylinder">
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<radius unit="M"> 1.24 </radius>
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<length unit="M"> 4.95 </length>
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</form>
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<pointmass name="PAX 0A (60 seats)">
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<weight unit="LBS">6600</weight> <!-- MAX: 13200lbs, 60 seats -->
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<location name="POINTMASS" unit="IN">
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<!-- #REF-1 page 88+98,
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x= (door form nose(8.16m))-(door with(1.816m)/2)+(Cargo compartment lenght(4.953m)/2)
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x= 9.7285 meters = 383.011811 in
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-->
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<x>383.01</x>
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<x>450.1711</x>
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<y>0</y>
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<z>-59.05</z> <!-- Aprox lower deck 1.5 meters = 59.0551181 in -->
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<z>0</z>
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</location>
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</pointmass>
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<pointmass name="Aft Cargo">
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<weight unit="LBS">0</weight> <!-- #REF-3 page 19, MAX 4536 kilograms = 10000.1682 lbs -->
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<form shape="cylinder">
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<radius unit="M"> 1.24 </radius>
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<length unit="M"> 6.6 </length>
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</form>
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<pointmass name="PAX 0B (60 seats)">
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<weight unit="LBS">6600</weight> <!-- MAX: 13200lbs, 60 seats -->
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<location name="POINTMASS" unit="IN">
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<!-- #REF-1 page 88+98,
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x= (door form nose(22.69m))-(door with(1.816m)/2)
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x= 21.78200 meters = 857.559055 in
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-->
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<x>857.55</x>
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<x>739.5669</x>
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<y>0</y>
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<z>-59.05</z> <!-- Aprox lower deck 1.5 meters = 59.0551181 in -->
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<z>0</z>
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</location>
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</pointmass>
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<pointmass name="Rear Bulk Cargo">
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<weight unit="LBS">0</weight> <!-- #REF-3 page 19, MAX 1497 kilograms = 3300.32006 lbs -->
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<form shape="cylinder">
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<radius unit="M"> 1.24 </radius>
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<length unit="M"> 2 </length>
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</form>
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<pointmass name="PAX 0C (54 seats)">
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<weight unit="LBS">5940</weight> <!-- MAX: 11880lbs, 54 seats -->
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<location name="POINTMASS" unit="IN">
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<!-- #REF-1 page 88+102,
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x= (door form nose(22.69m))+(door with(1.816m)/2)+( Dist. between rear doors(2.19))+(Aprox to compartment center (2m))
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x= 27.78800 meters = 1 094.01575 in
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-->
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<x>1094</x>
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<x>1093.2729</x>
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<y>0</y>
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<z>-39.37</z> <!-- Aprox bulk lower deck 1 meter = 39.3700787 in -->
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<z>0</z>
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</location>
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</pointmass>
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<pointmass name="Engine1">
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<weight unit="LBS">5248</weight>
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<form shape="cylinder">
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<radius unit="M"> 1.31 </radius>
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<length unit="M"> 5 </length>
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</form>
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<pointmass name="Cargo Hold 1">
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<weight unit="LBS">2000</weight> <!-- MAX: 7500.126lbs -->
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<location name="POINTMASS" unit="IN">
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<x>589.735</x>
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<y>-226.575</y>
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<z>-45.567</z>
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<x>383.4792</x>
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<y>0</y>
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<z>-29.5</z> <!-- 1.5m and now half of it for the center point of the load -->
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</location>
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</pointmass>
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<pointmass name="Engine2">
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<weight unit="LBS">5248</weight>
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<form shape="cylinder">
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<radius unit="M"> 1.31 </radius>
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<length unit="M"> 5 </length>
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</form>
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<!-- Cargo Hold 2 doesn't exist, that is the center tank -->
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<pointmass name="Cargo Hold 3">
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<weight unit="LBS">2000</weight> <!-- MAX: 5384.414lbs -->
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<location name="POINTMASS" unit="IN">
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<x>589.735</x>
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<y>226.575</y>
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<z>-45.567</z>
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<x>849.1324</x>
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<y>0</y>
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<z>-29.5</z>
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</location>
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</pointmass>
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<pointmass name="Cargo Hold 4">
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<weight unit="LBS">1500</weight> <!-- MAX: 4651.754lbs -->
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<location name="POINTMASS" unit="IN">
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<x>931.0653</x>
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<y>0</y>
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<z>-29.5</z>
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</location>
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</pointmass>
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<pointmass name="Cargo Hold 5">
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<weight unit="LBS">2000</weight> <!-- MAX: 3300.320lbs -->
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<location name="POINTMASS" unit="IN">
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<x>1068.2634</x>
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<y>0</y>
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<z>0</z> <!-- Cargo Hold #5 sits higher on the range of the cabin deck, it's only loadable with lifter -->
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</location>
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</pointmass>
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@ -430,6 +408,7 @@ YAW MOI_________3950000______23089847_______24848934
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</ground_reactions>
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<propulsion>
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<engine file="v2527_a5">
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<location unit="IN">
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<x> 589.735 </x>
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@ -457,6 +436,7 @@ YAW MOI_________3950000______23089847_______24848934
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</orient>
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</thruster>
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</engine>
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<engine file="v2527_a5">
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<location unit="IN">
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<x> 589.735 </x>
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@ -488,7 +468,7 @@ YAW MOI_________3950000______23089847_______24848934
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<tank type="FUEL"> <!-- Left Tank (Wing tip Ventilation Surge) 0 -->
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<location unit="IN">
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<x> 788.4322 </x>
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<x> 783.0709 </x>
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<y> -574.4148 </y>
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<z> 3.1080 </z>
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</location>
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@ -501,11 +481,11 @@ YAW MOI_________3950000______23089847_______24848934
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</tank>
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<tank type="FUEL"> <!-- Left Tank (Outer) 1 -->
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<location unit="IN">
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<x> 737.4190 </x>
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<x> 739.5669 </x>
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<y> -457.4259 </y>
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<z> -8.0898 </z>
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</location>
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<capacity unit="LBS"> 1548.8 </capacity><!-- need review -->
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<capacity unit="LBS"> 1520.00 </capacity><!-- need review -->
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<contents unit="LBS"> 154.88 </contents>
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<standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
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<priority>2</priority>
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@ -514,12 +494,12 @@ YAW MOI_________3950000______23089847_______24848934
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</tank>
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<tank type="FUEL"> <!-- Left Tank (Inner) 2 -->
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<location unit="IN">
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<x> 630.6588 </x>
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<x> 652.5591 </x>
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<y> -236.2992 </y>
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<z> -33.9470 </z>
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</location>
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<capacity unit="LBS"> 12186.9 </capacity><!-- need review -->
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<contents unit="LBS"> 2437.38 </contents>
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<capacity unit="LBS"> 11982 </capacity><!-- need review -->
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<contents unit="LBS"> 11982 </contents>
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<standpipe unit="LBS">31</standpipe><!-- minimun fuel on pipes -->
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<priority>3</priority>
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<type>JET-A1</type>
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@ -527,12 +507,12 @@ YAW MOI_________3950000______23089847_______24848934
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</tank>
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<tank type="FUEL"> <!-- Center Tank 3 -->
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<location unit="IN">
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<x> 580.9955 </x>
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<x> 522.0473 </x>
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<y> 0 </y>
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<z> -47.0 </z>
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</location>
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<capacity unit="LBS"> 14520 </capacity><!-- need review -->
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<contents unit="LBS"> 0 </contents>
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<capacity unit="LBS"> 14281 </capacity><!-- need review -->
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<contents unit="LBS"> 7260 </contents>
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<standpipe unit="LBS">43</standpipe><!-- minimun fuel on pipes -->
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<priority>1</priority>
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<type>JET-A1</type>
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@ -540,24 +520,24 @@ YAW MOI_________3950000______23089847_______24848934
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</tank>
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<tank type="FUEL"> <!-- Right Tank (Inner) 4 -->
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<location unit="IN">
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<x> 630.6588 </x>
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<x> 652.5591 </x>
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<y> 236.2992 </y>
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<z> -33.9470 </z>
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</location>
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<capacity unit="LBS"> 12186.9 </capacity><!-- need review -->
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<contents unit="LBS"> 2437.38 </contents>
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<standpipe unit="LBS">31</standpipe><!-- minimun fuel on pipes -->
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<capacity unit="LBS"> 11982 </capacity><!-- need review -->
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<contents unit="LBS"> 11982 </contents>
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<standpipe unit="LBS">31</standpipe><!-- minimum fuel on pipes -->
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<priority>3</priority>
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<type>JET-A1</type>
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<temperature>50</temperature>
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</tank>
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<tank type="FUEL"> <!-- Right Tank (Outer) 5 -->
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<location unit="IN">
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<x> 737.4190 </x>
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<x> 739.5669 </x>
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<y> 457.4259 </y>
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<z> -8.0898 </z>
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</location>
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<capacity unit="LBS"> 1548.8 </capacity><!-- need review -->
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<capacity unit="LBS"> 1520 </capacity><!-- need review -->
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<contents unit="LBS"> 154.88 </contents>
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<standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
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<priority>2</priority>
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@ -566,7 +546,7 @@ YAW MOI_________3950000______23089847_______24848934
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</tank>
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<tank type="FUEL"> <!-- Right Tank (Wing tip Ventilation Surge) 6 -->
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<location unit="IN">
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<x> 788.4322 </x>
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<x> 783.0709 </x>
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<y> 574.4148 </y>
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<z> 3.1080 </z>
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</location>
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968
A320-200-IAE.xml
968
A320-200-IAE.xml
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