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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: J79-GE-11A.xml Author: Aero-Matic v 0.8 Inputs: name: J79-GE-11A type: turbine thrust: 10000.0 lb augmented? yes injected? no --> <turbine_engine name="J79"> <milthrust> 10000.0 </milthrust> <maxthrust> 15800.0 </maxthrust> <bypassratio> 0.0 </bypassratio> <tsfc> 0.98 </tsfc> <atsfc> 1.96 </atsfc> <idlen1> 0.0 </idlen1> <idlen2> 53.0 </idlen2> <maxn1> 100.0 </maxn1> <maxn2> 100.0 </maxn2> <augmented> 1 </augmented> <augmethod> 1 </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 0.0 0.0430 0.0488 0.0528 0.0694 0.0899 0.1183 0.1467 0.2 0.0500 0.0501 0.0335 0.0544 0.0797 0.1049 0.1342 0.4 0.0040 0.0047 0.0020 0.0272 0.0595 0.0891 0.1203 0.6 0.0 0.0 0.0 0.0 0.0276 0.0718 0.1073 0.8 0.0 0.0 0.0 0.0 0.0474 0.0868 0.0900 1.0 0.0 0.0 0.0 0.0 0.0 0.0552 0.0800 </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 0.0 1.2600 1.0000 0.7400 0.5340 0.3720 0.2410 0.1490 0.2 1.1710 0.9340 0.6970 0.5060 0.3550 0.2310 0.1430 0.4 1.1500 0.9210 0.6920 0.5060 0.3570 0.2330 0.1450 0.6 1.1810 0.9510 0.7210 0.5320 0.3780 0.2480 0.1540 0.8 1.2580 1.0200 0.7820 0.5820 0.4170 0.2750 0.1700 1.0 1.3690 1.1200 0.8710 0.6510 0.4750 0.3150 0.2050 1.2 1.4850 1.2300 0.9750 0.7440 0.5980 0.3990 0.2450 1.4 1.5941 1.3400 1.0860 0.8450 0.7380 0.5340 0.2930 2.4 2.1396 1.8900 1.6410 1.3500 1.0430 0.7240 0.4530 </tableData> </table> </function> <function name="AugThrust"> <table> <independentVar lookup="row">velocities/mach</independentVar> <independentVar lookup="column">atmosphere/density-altitude</independentVar> <tableData> -10000 0 10000 20000 30000 40000 50000 0.0 1.1816 1.0000 0.8184 0.6627 0.5280 0.3756 0.2327 0.2 1.1308 0.9599 0.7890 0.6406 0.5116 0.3645 0.2258 0.4 1.1150 0.9474 0.7798 0.6340 0.5070 0.3615 0.2240 0.6 1.1284 0.9589 0.7894 0.6420 0.5134 0.3661 0.2268 0.8 1.1707 0.9942 0.8177 0.6647 0.5309 0.3784 0.2345 1.0 1.2411 1.0529 0.8648 0.7017 0.5596 0.3983 0.2467 1.2 1.3287 1.1254 0.9221 0.7462 0.5936 0.4219 0.2614 1.4 1.4365 1.2149 0.9933 0.8221 0.6360 0.4709 0.2994 1.6 1.5711 1.3260 1.0809 0.8900 0.6974 0.5060 0.3311 1.8 1.7301 1.4579 1.1857 0.9712 0.7595 0.5489 0.3777 2.0 1.8314 1.5700 1.3086 1.0774 0.8316 0.5986 0.3985 2.2 1.9700 1.6900 1.4100 1.2700 0.9300 0.6559 0.4340 2.4 2.0700 1.8000 1.5300 1.3700 1.0300 0.7500 0.4900 2.6 2.2000 1.9200 1.6400 1.4800 1.1400 0.8400 0.5600 </tableData> </table> </function> </turbine_engine>