jsbsim.js
Version:
JSBSim flight dynamics model ported to JavaScript
62 lines (55 loc) • 2.26 kB
text/xml
<!--
File: BR700-725.xml
Author: Aero-Matic v 0.81
Inputs:
name: BR700-725
type: turbine
thrust: 15460 lb
augmented? no
injected? no
-->
<turbine_engine name="BR700-725">
<milthrust> 15460.0 </milthrust>
<bypassratio> 4.4 </bypassratio>
<tsfc> 0.657 </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>