60 lines
2.1 KiB
XML
60 lines
2.1 KiB
XML
<?xml version="1.0"?>
|
|
<!--
|
|
File: V2522_A5.xml
|
|
Author: Aero-Matic v 0.81
|
|
|
|
Inputs:
|
|
name: V2522_A5
|
|
type: turbine
|
|
thrust: 21998.928 lb
|
|
augmented? no
|
|
injected? no
|
|
-->
|
|
|
|
<turbine_engine name="V2527_A5">
|
|
<milthrust> 26600 </milthrust>
|
|
<bypassratio> 2.0 </bypassratio>
|
|
<tsfc> 0.8 </tsfc>
|
|
<bleed> 0.03</bleed>
|
|
<idlen1> 23.4 </idlen1>
|
|
<idlen2> 63.7 </idlen2>
|
|
<maxn1> 105.8 </maxn1>
|
|
<maxn2> 112.5 </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
|
|
0.0 0.0430 0.0488 0.0528 0.0694 0.0899 0.1183 0.1467
|
|
0.2 0.0500 0.0501 0.0335 0.0544 0.0797 0.1049 0.1342
|
|
0.4 0.0040 0.0047 0.0020 0.0272 0.0595 0.0891 0.1203
|
|
0.6 0.0 0.0 0.0 0.0 0.0276 0.0718 0.1073
|
|
0.8 0.0 0.0 0.0 0.0 0.0474 0.0868 0.0900
|
|
1.0 0.0 0.0 0.0 0.0 0.0 0.0552 0.0800
|
|
</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
|
|
0.0 1.2600 1.0000 0.7400 0.5340 0.3720 0.2410 0.1490
|
|
0.2 1.1710 0.9340 0.6970 0.5060 0.3550 0.2310 0.1430
|
|
0.4 1.1500 0.9210 0.6920 0.5060 0.3570 0.2330 0.1450
|
|
0.6 1.1810 0.9510 0.7210 0.5320 0.3780 0.2480 0.1540
|
|
0.8 1.2580 1.0200 0.7820 0.5820 0.4170 0.2750 0.1700
|
|
1.0 1.3690 1.1200 0.8710 0.6510 0.4750 0.3150 0.1950
|
|
1.2 1.4850 1.2300 0.9750 0.7440 0.5450 0.3640 0.2250
|
|
1.4 1.5941 1.3400 1.0860 0.8450 0.6280 0.4240 0.2630
|
|
</tableData>
|
|
</table>
|
|
</function>
|
|
|
|
</turbine_engine>
|