jsbsim.js
Version:
JSBSim flight dynamics model ported to JavaScript
75 lines (68 loc) • 2 kB
text/xml
<!-- Generated by Aero-Matic v 0.8
Inputs:
horsepower: 1650.0
pitch: variable
max engine rpm: 2700
prop diameter (ft): 11
Outputs:
max prop rpm:1705.73
gear ratio: 1.58
Cp0: 0.103133
Ct0: 0.088694
static thrust (lbs):2495.71
-->
<propeller name="prop">
<ixx>20.6680 </ixx>
<diameter unit="IN">132.0 </diameter>
<numblades> 4 </numblades>
<gearratio>1.58 </gearratio>
<minpitch> 12 </minpitch>
<maxpitch> 30 </maxpitch>
<minrpm> 1365 </minrpm>
<maxrpm> 1706 </maxrpm>
<table name="C_THRUST" type="internal">
<tableData>
12 30
0.0 0.0887 0.1287
0.1 0.0813 0.1287
0.2 0.0739 0.1287
0.3 0.0614 0.1281
0.4 0.0467 0.1274
0.5 0.0318 0.1257
0.6 0.0137 0.1190
0.7 -0.0012 0.1071
0.8 -0.0262 0.0950
1.0 -0.0569 0.0632
1.2 -0.0931 0.0337
1.4 -0.1274 0.0024
1.6 -0.1667 -0.0277
1.8 -0.2040 -0.0577
2.0 -0.2395 -0.0891
2.2 -0.2750 -0.1210
2.4 -0.3104 -0.1531
</tableData>
</table>
<table name="C_POWER" type="internal">
<tableData>
12 30
0.0 0.1031 0.1631
0.1 0.1031 0.1631
0.2 0.0983 0.1631
0.3 0.0934 0.1631
0.4 0.0822 0.1631
0.5 0.0677 0.1613
0.6 0.0548 0.1595
0.7 0.0323 0.1560
0.8 0.0129 0.1486
1.0 -0.0387 0.1214
1.2 -0.1127 0.0816
1.4 -0.2094 0.0408
1.6 -0.3094 -0.0036
1.8 -0.4125 -0.0995
2.0 -0.5157 -0.1990
2.2 -0.6188 -0.2985
2.4 -0.7219 -0.3980
</tableData>
</table>
</propeller>