jsbsim.js
Version:
JSBSim flight dynamics model ported to JavaScript
61 lines (55 loc) • 2.24 kB
text/xml
<!--
File: J52.xml
Author: Aero-Matic v 0.8
Inputs:
name: J52
type: turbine
thrust: 11200.0 lb
augmented? no
injected? no
-->
<turbine_engine name="J52">
<milthrust> 11200.0 </milthrust>
<bypassratio> 1.0 </bypassratio>
<tsfc> 0.8 </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>