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Ryan-PT21-A-yasim.xml
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Ryan-PT21-A-yasim.xml
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<?xml version="1.0" encoding="UTF-8"?>
<!-- Ryan PT 22 : 2009 BARANGER Emmanuel
source : http://en.wikipedia.org/wiki/PT-22_Recruit
http://www.aerospacemuseum.org/exhibits/aircraft_april.html
Envergure : 10.17 m ( 30 ft 1.0 in )
Longueur : 6.9 m ( 22 ft 7.5 in )
Hauteur : 2.88 m ( 7 ft 2.0 in )
Empty weight : 683.68 kg ( 1507 lbs )
Cruise speed : 160.93 km/h ( 95 kts )
Moteur : Kinner R-811, 240 cv
-->
<airplane mass="1407">
<approach speed="44" aoa="5" fuel="0.2">
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.12"/>
<control-setting axis="/controls/engines/engine[0]/mixture" value="1.0"/>
<control-setting axis="/controls/flight/flaps" value="0.5"/>
</approach>
<cruise speed="90" alt="9000">
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.72"/>
<control-setting axis="/controls/engines/engine[0]/mixture" value="0.68"/>
<control-setting axis="/controls/flight/flaps" value="0.0"/>
</cruise>
<cockpit x="0.050" y="0" z="0.632"/>
<fuselage ax="3.4019" ay="0" az="0.1201" bx="2.598" by="0" bz="0.1201" width="0.88" taper="0.05" midpoint="1.0"/>
<fuselage ax="2.598" ay="0" az="0.1201" bx="-0.2206" by="0" bz="0.128" width="0.907" taper="1.0" midpoint="0.5" cy="2.92" cz="2.995"/>
<fuselage ax="-0.2206" ay="0" az="0.128" bx="-3.261" by="0" bz="0.009" width="0.887" taper="0.062" midpoint="0.0" cy="2.88" cz="2.174"/>
<wing x="0.965" y="0.3305" z="-0.2245"
chord="1.447"
length="4.2632"
taper="1"
incidence="1.25"
dihedral="5"
sweep="4.2"
camber="0.092"
wash="0.56">
<stall aoa="17" width="4" peak="1.65"/>
<flap0 start="0.092" end="0.40" lift="1.5" drag="1.82"/>
<flap1 start="0.520" end="1.000" lift="1.32" drag="1.13"/>
<control-input axis="/controls/flight/flaps" control="FLAP0"/>
<control-speed control="FLAP0" transition-time="5"/>
<control-output control="FLAP0" prop="/surface-positions/flaps-pos-norm"/>
<control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
<control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true"/>
<control-output control="FLAP1" side="left" prop="/surface-positions/left-aileron-pos-norm"/>
<control-output control="FLAP1" side="right" prop="/surface-positions/right-aileron-pos-norm"/>
</wing>
<mstab x="1.1915" y="0.0" z="0.9915"
chord="1.467"
length="4.823"
taper="1"
incidence="1.25"
dihedral="5"
sweep="4.2"
camber="0.092"
wash="0.4">
</mstab>
<hstab x="-2.522" y="0" z="0.118"
chord="1.258"
length="1.453"
taper="0.56"
wash="0.66">
<stall aoa="17" width="4" peak="1.5"/>
<flap0 start="0" end="1" lift="1.68" drag="1.18"/>
<control-input axis="/controls/flight/elevator" control="FLAP0"/>
<control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
</hstab>
<vstab x="-2.642" y="0" z="0.112"
chord="1.822"
length="1.63"
sweep="10"
effectiveness="1.23"
taper="0.55"
wash="0.53">
<stall aoa="15" width="4" peak="1.5"/>
<flap0 start="-0.27" end="1.0" lift="1.53" drag="1.22"/>
<control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/>
<control-input axis="/controls/flight/rudder-trim" control="FLAP0" invert="true"/>
<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>
</vstab>
<!-- Engines source : http://en.wikipedia.org/wiki/Kinner_K-5
http://wapedia.mobi/en/Kinner_R-5
name : Kinner R-730
type : five cylinder radial engine
power cruise : 240hp at 1,900 RPM max / 173hp at 1,600 RPM cruise
weight : 330lb (149.6 kg)
Displacement : 811cu in (13.29 L)
Compression : 5.50:1
Propeller diameter: 2.6 m
-->
<propeller x="2.967" y="0" z="0.161"
radius="1.275"
mass="370"
moment="8"
cruise-alt="7000"
cruise-power="173"
cruise-speed="90"
cruise-rpm="1700"
takeoff-rpm="1900"
takeoff-power="240">
<actionpt x="3.324" y="0" z="0.161"/>
<piston-engine eng-power="240"
eng-rpm="1900"
bore="5.75"
stroke="6.25"
min-throttle="0.065"
displacement="811.48"
compression="5.50">
<control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[0]/starter" control="STARTER"/>
<control-input axis="/controls/engines/engine[0]/magnetos" control="MAGNETOS"/>
<control-input axis="/controls/engines/engine[0]/mixture" control="MIXTURE"/>
</piston-engine>
</propeller>
<gear x="1.8526" y="0.989" z="-1.495"
compression="0.29"
spring="1.26"
damp="0.52"
dfric="0.96"
sfric ="0.40">
<control-input axis="/controls/gear/brake-left" control="BRAKE"/>
<control-input axis="/controls/gear/brake-parking" control="BRAKE"/>
</gear>
<gear x="1.8526" y="-0.989" z="-1.495"
compression="0.29"
spring="1.26"
damp="0.52"
dfric="0.96"
sfric ="0.40">
<control-input axis="/controls/gear/brake-right" control="BRAKE"/>
<control-input axis="/controls/gear/brake-parking" control="BRAKE"/>
</gear>
<gear x="-2.664" y="0" z="-0.49"
compression="0.09"
spring="0.46"
damp="0.52"
dfric="1.26"
sfric ="0.40">
<control-input axis="/controls/flight/rudder" control="STEER" src0="-1.0" src1="1.0" dst0="0.55" dst1="-0.55"/>
</gear>
<!-- Pilot Weight -->
<weight x="0.05" y="0.00" z=" 0.0113" mass-prop="/sim/weight[0]/weight-lb"/>
<weight x="1.1628" y="0.00" z=" 0.03" mass-prop="/sim/weight[1]/weight-lb"/>
<tank x="2.101" y="0.000" z="0.075" capacity="254"/>
<!-- CG theory x=0.975 y=0 z=-0.293 -->
<ballast x="-0.13" y="0" z="-0.09" mass="300"/>
</airplane>