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jsbsim.js

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JSBSim flight dynamics model ported to JavaScript

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<?xml version="1.0"?> <!-- 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>