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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"?> <!-- File: CFM56_5.xml Author: Aero-Matic v 0.8 Inputs: name: CFM56_5 type: turbine thrust: 25000 lb augmented? no injected? no --> <turbine_engine name="CFM56_5"> <milthrust> 25000.0 </milthrust> <bypassratio> 5.9 </bypassratio> <tsfc> 0.657 </tsfc> <idlen1> 30.0 </idlen1> <idlen2> 60.0 </idlen2> <maxn1> 100.0 </maxn1> <maxn2> 100.0 </maxn2> <augmented> 0 </augmented> <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 0.0420 0.0436 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 0.0174 0.0468 0.0900 0.0 1.0 0.0 0.0 0.0 0.0 0.0 0.0422 0.0700 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 1.0 1.3690 1.1200 0.8710 0.6510 0.4750 0.3150 0.1950 0.0 1.2 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0 </tableData> </table> </function> </turbine_engine>