jsbsim.js
Version:
JSBSim flight dynamics model ported to JavaScript
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text/xml
<!--
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>