You were looking from a bad angle. Radar and winglets are wanted by bounty maintainer. Everybody is a critic.
Update: I've fixed the right winglet angle/length, cockpit wall thicknes, cannon turret and made a new main rotor. Thanks for sugestions!
pjedvaj wrote in Thu Feb 09, 2012 8:37 pm:Issues: tail rotor isn't working (spinning) and I probably need to add some balast mass. It's flying a paper weight!
<!-- Boeing-Sikorsky RAH-66 Commanche
http://pjedvaj.eu5.org (pjedvaj FlightGear)
Petar Jedvaj, adapted from HHS's Kawasaki OH-1 Ninja -->
<!-- Empty weight -->
<airplane mass="9300">
<!-- Performance -->
<approach speed="60">
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.3"/>
</approach>
<cruise speed="165" alt="100">
<control-setting axis="/controls/engines/engine[0]/throttle" value="1.0"/>
</cruise>
<!-- Powerplant (2x LHTEC T800-LHT-801) -->
<!-- Main rotor -->
<rotor name="main" x="1.09" y="0.0" z="3.36" nx="0.043" ny="0" nz="0.999" fx="0.99" fy="0" fz="-0.043" ccw="1" phi0="45"
maxcollective="15.0" mincollective="0.2"
mincyclicail="-6" maxcyclicail="4"
mincyclicele="-4.7" maxcyclicele="14.5"
diameter="11.9" numblades="5" weightperblade="60" relbladecenter="0.5"
dynamic="1" rpm="355" rellenflaphinge="0.2" delta3="0.0"
delta=".25"
pitch-a="10"
pitch-b="15"
flapmin="-13.0"
flapmax="13.0"
flap0="-2.0"
flap0factor="0"
notorque="0"
dragfactor="0.30"
translift-ve="20"
translift-maxfactor="1.3"
ground-effect-constant="0.1"
twist="-8.5"
taper="1"
chord="0.38"
number-of-segments="8"
number-of-parts="8"
rel-len-where-incidence-is-measured="0.7"
rel-len-blade-start="0.076"
airfoil-lift-coefficient="3.55"
airfoil-drag-coefficient0="0.0150"
airfoil-drag-coefficient1="0.25"
incidence-stall-zero-speed="13"
incidence-stall-half-sonic-speed="12.5"
lift-factor-stall="0.18"
stall-change-over="5.5"
drag-factor-stall="2.0"
cyclic-factor="1.0"
rotor-correction-factor="0.9">
<control-input axis="/controls/flight/aileron-trim" control="CYCLICAIL" split="true"/>
<control-input axis="/controls/flight/fcs/roll" control="CYCLICAIL"
src0="-1.0" src1="1.0"
dst0="-1.0" dst1="1.0"/>
<control-input axis="/controls/flight/elevator-trim" control="CYCLICELE" split="true"/>
<control-input axis="/controls/flight/fcs/pitch" control="CYCLICELE"
src0="-1.0" src1="1.0"
dst0="-1.0" dst1="1.0"/>
<control-input axis="/controls/engines/engine[0]/throttle" control="COLLECTIVE"
src0="0.0" src1="1.0"
dst0="1.0" dst1="-1.0"/>
</rotor>
<!-- Tail rotor -->
<rotor name="tail" x="-5.47" y="0.09" z="1.53" nx="0.07" ny="-1" nz="-0.05" fx="1" fy="0" fz="0" ccw="1"
maxcollective="15" mincollective="-9.5"
diameter="1.37" numblades="8" weightperblade="1" relbladecenter="0.7"
dynamic="1" rpm="3584" rellenflaphinge="0.0" delta3="0" translift="0" delta="0.5"
pitch-a="10"
pitch-b="15"
airfoil-lift-coefficient="6.4"
airfoil-drag-coefficient0="0.0035"
airfoil-drag-coefficient1="0.10"
notorque="0"
taper="1"
chord="0.205"
number-of-segments="5"
number-of-parts="4"
rel-len-blade-start="0.4"
incidence-stall-zero-speed="16"
incidence-stall-half-sonic-speed="18"
lift-factor-stall="0.18"
stall-change-over="5.5"
drag-factor-stall="8"
rotor-correction-factor="0.7">
<control-input axis="/controls/flight/fcs/yaw" control="COLLECTIVE" invert="true"
src0="-1.0" src1="1.0"
dst0="-1.0" dst1="1.0"/>
<control-input axis="/controls/flight/fcs/tail-rotor/throttle" control="COLLECTIVE"
src0="-1.0" src1="1.0"
dst0="-1.0" dst1="1.0"/>
</rotor>
<!-- Rotor gear -->
<rotorgear
max-power-engine="3126"
max-power-rotor-brake="100"
rotorgear-friction="1.4"
engine-prop-factor="0.005"
engine-accel-limit="2.96"
yasimdragfactor="12.5"
yasimliftfactor="170">
<control-input axis="/controls/engines/engine[0]/magnetos" control="ROTORGEARENGINEON"/>
<control-input axis="/controls/rotor/brake" control="ROTORBRAKE"
src0="0.0" src1="1.0"
dst0="0.0" dst1="1.0"/>
</rotorgear>
<!-- Airframe -->
<!-- Cockpit -->
<cockpit x="3.06" y="0" z="2.40"/>
<!-- Fuselage -->
<fuselage ax="5.85" ay="0" az="1.46" bx="-6.95" by="0" bz="1.30"
width="1.98" taper="0.5" midpoint="0.54"/>
<!-- Vertical stabilizer -->
<vstab x="-4.96" y="0" z="2.40" taper="0.5" length="1.60" chord="1.35" sweep="50" incidence="5">
<stall aoa="16" width="4" peak="1.5"/>
</vstab>
<!-- Horizontal stabilizer -->
<hstab x="-6.10" y="0" z="3.42" taper="1.0" effectiveness="0.6" length="1.35" chord="0.8" sweep="0" incidence="-5">
<stall aoa="20" width="5" peak="1.5"/>
<flap0 start="0.0" end="1.0" lift="1.6" drag="1.6"/>
<control-input axis="/controls/flight/fcs/stabilator" control="FLAP0"/>
</hstab>
<!-- Landing gear -->
<!-- Left gear -->
<gear x="2.47" y="0.89" z="0.27" retract-time="6" compression="0.30" spring="0.7" damp="2.8" sfric="1.4" dfric="0.9" on-water="0" on-solid="1">
<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-speed control="EXTEND" transition-time="7"/>
<control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>
</gear>
<!-- Right gear -->
<gear x="2.47" y="-0.89" z="0.27" retract-time="6" compression="0.30" spring="0.7" damp="2.8" sfric="1.4" dfric="0.9" on-water="0" on-solid="1">
<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-speed control="EXTEND" transition-time="7"/>
<control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>
</gear>
<!-- Tail gear -->
<gear x="-4.51" y="0.00" z="0.16" retract-time="6" compression="0.3" spring="0.7" damp="2.8" sfric="1.6" dfric="0.9" on-water="0" on-solid="1"/>
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-speed control="EXTEND" transition-time="7"/>
<control-output control="EXTEND" prop="/gear/gear[2]/position-norm"/>
<!-- Fuel tank -->
<tank x="1.09" y="0" z="1.53" capacity="1918"/>
<!-- Weights -->
<!-- Ballast -->
<ballast x="2.24" y="0.0" z="-1.66" mass="1550"/>
<ballast x="0.24" y="0.0" z="-1.66" mass="1550"/>
<ballast x="1.24" y="0.0" z="-1.66" mass="1550"/>
<ballast x="1.24" y="0.0" z="-1.66" mass="1550"/>
<ballast x="1.24" y="0.0" z="-1.66" mass="1550"/>
<ballast x="1.24" y="0.0" z="-1.66" mass="1550"/>
<!-- Pilot -->
<weight x="3.63" y="0" z="1.83" mass-prop="/sim/weight[0]/weight-lb"/>
<!-- Gunner -->
<weight x="2.31" y="0" z="2.10" mass-prop="/sim/weight[1]/weight-lb"/>
<!-- Armament -->
<weight x="1.04" y="-1.09" z="1.33" size="0.18" mass-prop="sim/weight[6]/weight-lb"/>
<weight x="1.04" y="-1.32" z="1.39" size="0.18" mass-prop="sim/weight[4]/weight-lb"/>
<weight x="1.04" y="-1.56" z="1.33" size="0.18" mass-prop="sim/weight[2]/weight-lb"/>
<weight x="1.04" y="1.56" z="1.33" size="0.18" mass-prop="sim/weight[3]/weight-lb"/>
<weight x="1.04" y="1.32" z="1.39" size="0.18" mass-prop="sim/weight[5]/weight-lb"/>
<weight x="1.04" y="1.09" z="1.33" size="0.18" mass-prop="sim/weight[7]/weight-lb"/>
</airplane>
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