jsbsim.js
Version:
JSBSim flight dynamics model ported to JavaScript
76 lines (70 loc) • 2.02 kB
text/xml
<!-- Generated by Aero-Matic v 0.8
Inputs:
horsepower: 1200
pitch: variable
max engine rpm: 2500
prop diameter (ft): 11.583333333333
Outputs:
max prop rpm:1619.83
gear ratio: 1.54
Cp0:0.067641
Ct0:0.058172
static thrust (lbs):1815.06
-->
<propeller name="prop">
<ixx>35 </ixx>
<diameter unit="IN">139.0 </diameter>
<numblades> 3 </numblades>
<gearratio>1.54 </gearratio>
<minpitch> 12 </minpitch>
<maxpitch> 30 </maxpitch>
<minrpm> 1400 </minrpm>
<maxrpm> 1700 </maxrpm>
<ct_factor> 1.20 </ct_factor>
<cp_factor> 0.80 </cp_factor>
<table name="C_THRUST" type="internal">
<tableData>
12 30
0.0 0.0582 0.0982
0.1 0.0533 0.0982
0.2 0.0485 0.0982
0.3 0.0403 0.0977
0.4 0.0306 0.0972
0.5 0.0209 0.0959
0.6 0.0090 0.0908
0.7 -0.0008 0.0817
0.8 -0.0172 0.0725
1.0 -0.0373 0.0482
1.2 -0.0611 0.0257
1.4 -0.0835 0.0019
1.6 -0.1094 -0.0211
1.8 -0.1338 -0.0440
2.0 -0.1571 -0.0679
2.2 -0.1803 -0.0923
2.4 -0.2036 -0.1168
</tableData>
</table>
<table name="C_POWER" type="internal">
<tableData>
12 30
0.0 0.0676 0.1276
0.1 0.0676 0.1276
0.2 0.0645 0.1276
0.3 0.0613 0.1276
0.4 0.0539 0.1276
0.5 0.0444 0.1262
0.6 0.0359 0.1248
0.7 0.0212 0.1220
0.8 0.0085 0.1163
1.0 -0.0254 0.0950
1.2 -0.0739 0.0638
1.4 -0.1373 0.0319
1.6 -0.2029 -0.0028
1.8 -0.2706 -0.0779
2.0 -0.3382 -0.1557
2.2 -0.4058 -0.2336
2.4 -0.4735 -0.3114
</tableData>
</table>
</propeller>