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pa22-160-yasim.xml
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pa22-160-yasim.xml
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<?xml version="1.0"?>
<!--
********************************************************************************
Piper PA-22 "Tri-Pacer" for FlightGear
********************************************************************************
Authors: Robert Leda, Pawel Luchowski
License: GPL (see file "COPYING" for details)
********************************************************************************
Obtained from: https://sourceforge.net/p/flightgear/fgaddon/HEAD/tree/trunk/Aircraft/pa22/
Model PA-22-160
Engine Lyc O-320-B
Hp & RPM 160 @ 2700
Gross Weight (Lbs.) 2000
Empty Weight (Lbs.) 1110
Wingspan (Ft.) 29.3
Wing Area (Sq. Ft.) 147.5
Length Ft. 20.6
Height In. 100
Propeller Dia. In. 74
Power Loading Lbs./hp 12.5
Wing Loading Lbs./sq ft 13.5
Baggage Cap. Lbs. 100
Fuel Cap. US Gal. 36
Maximum Speed mph 141
Cruise mph:75% @ sl 125
Cruise mph:75% @ 7000 134
Stall Speed mph 49*
Takeoff Run ft. 1120*
Landing Roll ft. 500*
Rate of Climb ft/min 800
Service Ceiling ft 16,500
Cruising Range s/mi 500
* flaps down
-->
<airplane mass="1110">
<approach speed="65" aoa="2" fuel="0.2">
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.2"/>
<control-setting axis="/controls/engines/engine[0]/mixture" value="1.00"/>
<control-setting axis="/controls/flight/flaps" value="1.0"/>
</approach>
<cruise speed="116" alt="7000" fuel="0.2">
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.75"/>
<control-setting axis="/controls/engines/engine[0]/mixture" value="0.75"/>
<control-setting axis="/controls/flight/flaps" value="0.0"/>
</cruise>
<cockpit x="-0.32" y="0.18" z="0.57"/>
<fuselage ax="1.472" ay="0.0" az="0.09" bx="-3.926" by="0.0" bz="-0.12" width="1.003" taper="1.0" midpoint="0.36" idrag="0.9"/>
<!--real dihedral is about 2.5 -->
<wing x="-0.554" y="0.429" z="0.696" length="3.984" chord="1.608" incidence="2" dihedral="5.5" camber="0.04">
<stall aoa="18" width="2.0" peak="1.5"/>
<flap0 start="0.03" end="0.35" lift="1.4" drag="1.6"/>
<flap1 start="0.35" end="0.81" lift="1.3" drag="1.2"/>
<control-input axis="/controls/flight/flaps" control="FLAP0"/>
<control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
<control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true"/>
<control-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/>
<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"/>
<control-speed transition-time="4.0" control="FLAP0"/>
<control-speed transition-time="0.5" control="FLAP1"/>
</wing>
<hstab x="-3.833" y="0.03" z="0.264" length="1.421" chord="1.205" sweep="10">
<stall aoa="16" width="4.0" peak="1.5"/>
<flap0 start="0" end="1" lift="1.5" drag="1.4" effectiveness="2"/>
<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"/>
<control-speed transition-time="0.5" control="FLAP0"/>
</hstab>
<vstab x="-3.976" y="0.0" z="0.265" length="1.055" chord="1.373" sweep="36">
<stall aoa="16" width="4.0" peak="1.5"/>
<flap0 start="0" end="1" lift="1.3" drag="1.2"/>
<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" min="1" max="-1"/>
<control-speed transition-time="0.5" control="FLAP0"/>
</vstab>
<!-- engine: Lyc O-320-B2A -->
<!-- propeller: Sensenich 74DM6-0-60 -->
<!-- engine mass = 259, propeller mass = 32.4, wastegate-mp probably 35 or 45-->
<propeller x="1.080" y="0.002" z="-0.034" mass="291.4" moment="4" radius="0.9398" cruise-speed="126" cruise-rpm="2675" cruise-power="120" cruise-alt="7000" takeoff-power="160" takeoff-rpm="2700">
<piston-engine eng-power="160" eng-rpm="2700" displacement="320" compression="8.5" wastegate-mp="35"/>
<actionpt x="1.55" y="0.0" z="0.09" />
<control-input control="THROTTLE" axis="/controls/engines/engine[0]/throttle"/>
<control-input control="STARTER" axis="/controls/engines/engine[0]/starter"/>
<control-input control="MAGNETOS" axis="/controls/engines/engine[0]/magnetos"/>
<control-input control="MIXTURE" axis="/controls/engines/engine[0]/mixture"/>
</propeller>
<!-- nose -->
<gear x="1.197" y="0.0" z="-1.179" compression="0.16" spring="0.8">
<control-input axis="/controls/flight/rudder" control="STEER"
src0="-1.0" src1="1.0"
dst0="-0.1" dst1="0.1"/>
</gear>
<!-- left main -->
<gear x="-0.495" y="1.053" z="-1.129" compression="0.1" spring="0.8">
<control-input axis="/controls/gear/brake-left" control="BRAKE" split="true"/>
<control-input axis="/controls/gear/brake-parking" control="BRAKE" split="true"/>
</gear>
<!-- right main -->
<gear x="-0.495" y="-1.053" z="-1.129" compression="0.1" spring="0.8">
<control-input axis="/controls/gear/brake-right" control="BRAKE" split="true"/>
<control-input axis="/controls/gear/brake-parking" control="BRAKE" split="true"/>
</gear>
<tank x="-0.387" y="0.928" z="0.77" capacity="108"/>
<tank x="-0.387" y="-0.928" z="0.77" capacity="108"/>
<!-- CG reference point is about x=0.222, with operating range between
0.019 and 0.362. -->
<ballast x="0.66" y="0.0" z="-0.050" mass="350"/>
<!-- Pilot, copilot, left passenger, right passenger, baggage -->
<weight x="-0.311" y="0.223" z="0.0" mass-prop="/sim/weight[0]/weight-lb"/>
<weight x="-0.311" y="-0.223" z="0.0" mass-prop="/sim/weight[1]/weight-lb"/>
<weight x="-1.023" y="0.200" z="0.0" mass-prop="/sim/weight[2]/weight-lb"/>
<weight x="-1.023" y="-0.200" z="0.0" mass-prop="/sim/weight[3]/weight-lb"/>
<weight x="-1.480" y="0.0" z="0.0" mass-prop="/sim/weight[4]/weight-lb"/>
</airplane>