UNPKG

jsbsim.js

Version:

JSBSim flight dynamics model ported to JavaScript

60 lines (54 loc) 2.2 kB
<?xml version="1.0"?> <!-- File: JT9D-3.xml Author: Aero-Matic v 0.8, Darren Jones Inputs: name: JT9D-3 type: turbine thrust: 43500 lb augmented? no injected? no --> <turbine_engine name="JT9D-3"> <milthrust> 43500.0 </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> <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 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 1.2 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0 </tableData> </table> </function> </turbine_engine>