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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: BR710.xml Author: Aero-Matic v 0.81 Inputs: name: Rolls Royce BR710 type: turbine thrust: 15000 lb augmented? no injected? no reference: http://www.togo84.com/spec05_gas_turbines.pdf or: http://www.aviationnow.com/media/pdf/spec05_gas_turbines.pdf -------------------------------------------------------- type: .............................. A-F no. fan stages: .................... 1 no. compressor stages: ............. 10 no. turbine stages lp: ............. 2 no. turbine stages hp: ............. 2 compressor type: ................... An max power at sea level: ........... 15000 lb specific fuel consumption at max power: 0.639 overall pressure ratio at max power: 24 max envelope diameter: ............. 48 in max envelope length: ............... 134 in dirty weight (wo. tailpipe): ....... 3600 lb --> <turbine_engine name="BR710"> <milthrust> 15000.0 </milthrust> <bypassratio> 4.2 </bypassratio> <tsfc> 0.639 </tsfc> <bleed> 0.03</bleed> <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 0.0430 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 1.0 1.3690 1.1200 0.8710 0.6510 0.4750 0.3150 0.1950 0.0 1.2 1.4850 1.2300 0.9750 0.7440 0.5450 0.3640 0.2250 0.0 1.4 1.5941 1.3400 1.0860 0.8450 0.6280 0.4240 0.2630 0.0 </tableData> </table> </function> </turbine_engine>