jsbsim.js
Version:
JSBSim flight dynamics model ported to JavaScript
87 lines (80 loc) • 3.67 kB
text/xml
<!--
File: J79-GE-11A.xml
Author: Aero-Matic v 0.8
Inputs:
name: J79-GE-11A
type: turbine
thrust: 10000.0 lb
augmented? yes
injected? no
-->
<turbine_engine name="J79">
<milthrust> 10000.0 </milthrust>
<maxthrust> 15800.0 </maxthrust>
<bypassratio> 0.0 </bypassratio>
<tsfc> 0.95 </tsfc>
<atsfc> 1.90 </atsfc>
<idlen1> 0.0 </idlen1>
<idlen2> 53.0 </idlen2>
<maxn1> 100.0 </maxn1>
<maxn2> 100.0 </maxn2>
<augmented> 1 </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
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>
<function name="AugThrust">
<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 1.1816 1.0000 0.8184 0.6627 0.5280 0.3756 0.2327 0.0
0.2 1.1308 0.9599 0.7890 0.6406 0.5116 0.3645 0.2258 0.0
0.4 1.1150 0.9474 0.7798 0.6340 0.5070 0.3615 0.2240 0.0
0.6 1.1284 0.9589 0.7894 0.6420 0.5134 0.3661 0.2268 0.0
0.8 1.1707 0.9942 0.8177 0.6647 0.5309 0.3784 0.2345 0.0
1.0 1.2411 1.0529 0.8648 0.7017 0.5596 0.3983 0.2467 0.0
1.2 1.3287 1.1254 0.9221 0.7462 0.5936 0.4219 0.2614 0.0
1.4 1.4365 1.2149 0.9933 0.8021 0.6360 0.4509 0.2794 0.0
1.6 1.5711 1.3260 1.0809 0.8700 0.6874 0.4860 0.3011 0.0
1.8 1.7301 1.4579 1.1857 0.9512 0.7495 0.5289 0.3277 0.0
2.0 1.8314 1.5700 1.3086 1.0474 0.8216 0.5786 0.3585 0.0
2.2 1.9700 1.6900 1.4100 1.2400 0.9100 0.6359 0.3940 0.0
2.4 2.0700 1.8000 1.5300 1.3400 1.0000 0.7200 0.4600 0.0
2.6 2.2000 1.9200 1.6400 1.4400 1.1000 0.8000 0.5200 0.0
</tableData>
</table>
</function>
</turbine_engine>