Re: USA TOUR Event | SAT MARCH 5TH 17:00 - 24:00 UTC
Posted: Tue Feb 16, 2016 12:17 pm
If you'd like to try the DHC6, C172P, or PBY?
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<control-input axis="/controls/flight/rudder" control="STEER" square="true" src0="-1.0" src1="1.0" dst0="-1.5" dst1="1.5"/>
<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="5"/>
<!-- <control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-input axis="/controls/gear/tailwheel-lock" control="CASTERING"
src0="0" src1="1"
dst0="1" dst1="0"/>
<control-speed control="EXTEND" transition-time="5"/>
<control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/> -->
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<!-- Engine Wiki information: https://en.wikipedia.org/wiki/Wright_R-1820
Wright R-1820-32
General characteristics
Type: Nine-cylinder single-row supercharged air-cooled radial engine
Bore: 6.125 in (155.6 mm)
Stroke: 6.88 in (174.6 mm)
Displacement: 1,823 in3 (29.88 L)
Length: 47.76 in (1,213 mm)
Diameter: 54.25 in (1,378 mm)
Dry weight: 1,184 lb (537 kg)
Components
Valvetrain: Two overhead valves per cylinder with sodium-filled exhaust valve
Supercharger: Single-speed General Electric centrifugal type supercharger, blower ratio 7.134:1
Fuel system: Stromberg PD12K10 downdraft carburetor with automatic mixture control
Fuel type: 87 octane rating gasoline
Oil system: Dry sump with one pressure and one scavenging pump
Cooling system: Air-cooled
Performance
Power output: 1,000 hp (746 kW) at 2,300 rpm for takeoff
Specific power: 0.46 hp/in/3 (20.88 kW/L)
Compression ratio: 6.45:1
Specific fuel consumption: 0.6 lb/(hp*h) (362 g/(kW*h))
Oil consumption: 0.35-0.39 oz/(hp*h) (13-15 g/(kW*h))
Power-to-weight ratio: 0.84 hp/lb (1.39 kW/kg)
-->
<propeller x="-5.349" y="2.993" z="1.278"
radius="1.57"
mass="870"
moment="24.5"
blades="3"
cruise-alt="5000"
cruise-power="910"
cruise-speed="140"
cruise-rpm="1186"
gear-ratio="0.54"
min-rpm="500"
max-rpm="1242" >
<actionpt x="-4.688" y="2.993" z="1.342"/>
<control-input axis="/controls/engines/engine[0]/propeller-pitch" control="ADVANCE" />
<piston-engine
eng-power="1000"
eng-rpm="2300"
displacement="1823.2"
bore="6.125"
stroke="6.875"
min-throttle="0.067"
supercharger="1"
turbo-mul="1.46"
wastegate-mp="39.5"
compression-ratio="6.45"/>
<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"/>
<control-input axis="/controls/engines/engine[0]/boost" control="BOOST"/>
</propeller>
<propeller x="-5.349" y="-2.993" z="1.278"
radius="1.57"
mass="870"
moment="24.5"
blades="3"
cruise-alt="5000"
cruise-power="910"
cruise-speed="140"
cruise-rpm="1186"
gear-ratio="0.54"
min-rpm="500"
max-rpm="1242" >
<actionpt x="-4.688" y="-2.993" z="1.342"/>
<control-input axis="/controls/engines/engine[1]/propeller-pitch" control="ADVANCE" />
<piston-engine
eng-power="1000"
eng-rpm="2300"
displacement="1823.2"
bore="6.125"
stroke="6.875"
min-throttle="0.067"
supercharger="1"
turbo-mul="1.46"
wastegate-mp="39.5"
compression-ratio="6.45"/>
<control-input axis="/controls/engines/engine[1]/throttle" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[1]/starter" control="STARTER"/>
<control-input axis="/controls/engines/engine[1]/magnetos" control="MAGNETOS"/>
<control-input axis="/controls/engines/engine[1]/mixture" control="MIXTURE"/>
<control-input axis="/controls/engines/engine[0]/boost" control="BOOST"/>
</propeller>