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MD-90-yasim.xml
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<?xml version="1.0"?>
<!-- YASim Aerodynamic Model for the McDonnell Douglas MD-90 -->
<!-- Based on Andino's MD-82 -->
<!--
Specifications:
Empty: 88000 lbs
Zero Fuel: 118000 lbs
Max Fuel load: 39128 lbs
Max Payload: 40112 lbs
Max Take-Off: 156000 lbs
Max Land: 128000 lbs
Cruise: Mach 0.76 @ 35000'
-->
<airplane mass="88000">
<!-- Approach configuration -->
<approach speed="125" aoa="5" fuel="0.3">
<control-setting axis="/controls/engines/engine[0]/throttle-lever" value="0.4"/>
<control-setting axis="/controls/engines/engine[1]/throttle-lever" value="0.4"/>
<control-setting axis="/controls/flight/flaps" value="1.0"/>
<control-setting axis="/controls/flight/slats" value="1.0"/>
<control-setting axis="/controls/gear/gear-down" value="1"/>
<solve-weight idx="0" weight="360"/>
<solve-weight idx="1" weight="30000"/>
</approach>
<!-- Cruise configuration -->
<cruise speed="482" alt="35000" fuel="0.59">
<control-setting axis="/controls/engines/engine[0]/throttle-lever" value="0.86"/>
<control-setting axis="/controls/engines/engine[1]/throttle-lever" value="0.86"/>
<control-setting axis="/controls/flight/flaps" value="0.0"/>
<control-setting axis="/controls/flight/slats" value="0.0"/>
<control-setting axis="/controls/gear/gear-down" value="0"/>
<solve-weight idx="0" weight="360"/>
<solve-weight idx="1" weight="30000"/>
</cruise>
<!-- Pilot viewpoint -->
<cockpit x="-2.9" y="0.5" z="1.2"/>
<!-- Fuselage, essentially a nose cone + a body cylinder + a tail cone -->
<fuselage ax="0.0" ay="0.0" az="-0.263" bx="-5.087" by="0.0" bz="0.506"
width="3.328" taper="0.3" midpoint="1.0" />
<fuselage ax="-5.087" ay="0.0" az="0.506" bx="-32.160" by="0.0" bz="0.506"
width="3.328" taper="1.0" midpoint="0.5" />
<fuselage ax="-32.160" ay="0.0" az="0.506" bx="-41.889" by="0.0" bz="1.158"
width="3.328" taper="0.0" midpoint="0.0" />
<!-- Engine Nacelles, true width of 1.7 halved for a guess at effective drag width -->
<!-- Left engine -->
<fuselage ax="-30.845" ay="2.7" az="0.738" bx="-37.246" by="2.7" bz="0.516"
width="0.85" taper="0.5" midpoint="0.3" />
<!-- Right engine -->
<fuselage ax="-30.845" ay="-2.7" az="0.738" bx="-37.246" by="-2.7" bz="0.516"
width="0.85" taper="0.5" midpoint="0.3" />
<wing x="-22.25" y="1.630" z="-0.648"
length="15.632"
chord="6.308"
taper="0.17"
sweep="19"
dihedral="3"
incidence="1.5"
camber="0.1"
twist="-2.0">
<stall aoa="10" width="2" peak="1.5"/>
<flap0 start="0" end="0.597" lift="1.7" drag="2.2"/>
<flap1 start="0.597" end="0.824" lift="1.45" drag="1.5"/>
<slat start="0" end="1" aoa="3" drag="1.1"/>
<spoiler start="0.078" end="0.554" lift="0.7" drag="2.0"/>
<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-input axis="/controls/flight/slats" control="SLAT"/>
<control-input axis="/controls/flight/spoilers" control="SPOILER"/>
<control-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/>
<control-output control="SLAT" prop="/surface-positions/slat-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-output control="SPOILER" prop="/surface-positions/spoiler-pos-norm"/>
<control-speed control="FLAP0" transition-time="10"/>
<control-speed control="SLAT" transition-time="10"/>
<control-speed control="SPOILER" transition-time="1"/>
</wing>
<hstab x="-41.691" y="0.220" z="5.727"
length="6.520"
chord="3.602"
taper="0.392"
sweep="26.5"
dihedral="-3"
incidence="0"
camber="0">
<stall aoa="20" width="4" peak="1.5"/>
<flap0 start="0" end="1" lift="1.3" drag="1.3"/>
<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="-38.578" y="0" z="1.952"
length="5.185"
chord="4.507"
taper="0.928"
sweep="44">
<stall aoa="15" width="2" peak="1.5"/>
<flap0 start="0" end="0.829" lift="1.5" drag="1.5"/>
<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>
<!-- IAE V2500 D5 -->
<jet x="-33.757" y="2.7" z="0.687" mass="4567" thrust="25000" egt="625" tsfc="0.498" n1-idle="23.4" n2-idle="63.7" n1-max="105.8" n2-max="102.1" epr="1.49">
<control-input axis="/controls/engines/engine[0]/throttle-lever" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[0]/reverser" control="REVERSE_THRUST"/>
<control-output control="REVERSE_THRUST" prop="/surface-positions/reverser-norm[0]"/>
<control-speed control="REVERSE_THRUST" transition-time="1"/>
<actionpt x="-35.0" y="2.7" z="0.687"/>
</jet>
<jet x="-33.757" y="-2.7" z="0.687" mass="4567" thrust="25000" egt="625" tsfc="0.498" n1-idle="23.4" n2-idle="63.7" n1-max="105.8" n2-max="102.1" epr="1.49">
<control-input axis="/controls/engines/engine[1]/throttle-lever" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[1]/reverser" control="REVERSE_THRUST"/>
<control-output control="REVERSE_THRUST" prop="/surface-positions/reverser-norm[1]"/>
<control-speed control="REVERSE_THRUST" transition-time="1"/>
<actionpt x="-35.0" y="-2.7" z="0.687"/>
</jet>
<thruster x="19.246" y="0.00" z="-2.7" vx="1" vy="0" vz="0" thrust="8000">
<control-input axis="/sim/model/pushback/target-speed-fps" control="THROTTLE" src0="-1" src1="1" dst0="-1" dst1="1"/>
</thruster>
<!-- Gear -->
<!-- Nose -->
<gear x="-1.076" y="0" z="-2.451"
compression="0.38"
spring="0.5"
damp="4"
>
<control-input axis="/controls/flight/rudder" control="STEER" square="true"/>
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>
<control-speed control="EXTEND" transition-time="10"/>
</gear>
<!-- Left main -->
<gear x="-24.5" y="3.112" z="-2.949"
compression="0.55"
spring="0.35"
>
<control-input axis="/controls/gear/brake-left" control="BRAKE"/>
<control-input axis="/controls/gear/brake-parking" control="BRAKE" split="true"/>
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>
<control-speed control="EXTEND" transition-time="10"/>
</gear>
<!-- Right main -->
<gear x="-24.5" y="-3.112" z="-2.949"
compression="0.55"
spring="0.35"
>
<control-input axis="/controls/gear/brake-right" control="BRAKE"/>
<control-input axis="/controls/gear/brake-parking" control="BRAKE" split="true"/>
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-output control="EXTEND" prop="/gear/gear[2]/position-norm"/>
<control-speed control="EXTEND" transition-time="10"/>
</gear>
<tank x="-22.4" y="5.7" z="-0.465" capacity="9266" jet="true"/>
<tank x="-22.4" y="-5.7" z="-0.465" capacity="9266" jet="true"/>
<tank x="-22.4" y="0" z="-0.465" capacity="20596" jet="true"/>
<!-- Forward ballast for nose gear, batteries, avionics, etc. -->
<ballast x="-2.0" y="0.0" z="0.0" mass="7000.0" />
<!-- Some ballast for mass of main landing gear assemblies -->
<ballast x="-24.390" y="-2.0" z="-0.658" mass="3000.0" />
<ballast x="-24.390" y="2.0" z="-0.658" mass="3000.0" />
<weight x="-2.9" y="0.0" z="0.6" mass-prop="/sim/weight[0]/weight-lb"/> <!-- Crew -->
<!-- Crude initial positioning of cargo/passengers. Would like to itemize this by location later. -->
<weight x="-23.0" y="0.0" z="0.0" mass-prop="/sim/weight[1]/weight-lb"/> <!-- Cargo/Passengers -->
</airplane>