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jsbsim.js

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JSBSim flight dynamics model ported to JavaScript

github.com/csbrandt/JSBSim.js

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<?xml version="1.0"?> <!-- File: RollsRoyce.xml Author: Aero-Matic v 0.8, Luca Masera Inputs: name: RollsRoyce type: turbine thrust: 4500.316 lb augmented? no injected? no --> <turbine_engine name="RollsRoyce"> <milthrust> 4200.0 </milthrust> <bypassratio> 0.4 </bypassratio> <tsfc> 0.775 </tsfc> <idlen1> 40.0 </idlen1> <idlen2> 53.0 </idlen2> <maxn1> 105.0 </maxn1> <maxn2> 110.0 </maxn2> <augmented> 0 </augmented> <augmethod> 0 </augmethod> <injected> 0 </injected> <function name="IdleThrust"> <table> <independentVar lookup="row">velocities/mach</independentVar> <independentVar lookup="column">atmosphere/density-altitude</independentVar> <tableData> -10000 0 10000 20000 30000 40000 50000 60000 0.0 0.0430 0.0488 0.0528 0.0694 0.0899 0.1183 0.1467 0.0 0.2 0.0500 0.0501 0.0335 0.0544 0.0797 0.1049 0.1342 0.0 0.4 0.0040 0.0047 0.0020 0.0272 0.0595 0.0891 0.1203 0.0 0.6 0.0 0.0 0.0 0.0 0.0276 0.0718 0.1073 0.0 0.8 0.0 0.0 0.0 0.0 0.0474 0.0868 0.0900 0.0 1.0 0.0 0.0 0.0 0.0 0.0 0.0552 0.0800 0.0 </tableData> </table> </function> <function name="MilThrust"> <table> <independentVar lookup="row">velocities/mach</independentVar> <independentVar lookup="column">atmosphere/density-altitude</independentVar> <tableData> -10000 0 10000 20000 30000 40000 50000 60000 0.0 1.2600 1.0000 0.7400 0.5340 0.3720 0.2410 0.1490 0.0 0.2 1.1710 0.9340 0.6970 0.5060 0.3550 0.2310 0.1430 0.0 0.4 1.1500 0.9210 0.6920 0.5060 0.3570 0.2330 0.1450 0.0 0.6 1.1810 0.9510 0.7210 0.5320 0.3780 0.2480 0.1540 0.0 0.8 1.2580 1.0200 0.7820 0.5820 0.4170 0.2750 0.1700 0.0 0.95 1.3690 1.1200 0.8710 0.6510 0.4750 0.3150 0.1950 0.0 1.0 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0 </tableData> </table> </function> </turbine_engine>