<?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> 32000 </milthrust>
<bypassratio> 2.0 </bypassratio>
<tsfc> 0.8 </tsfc>
<bleed> 0.03</bleed>
<idlen1> 23.4 </idlen1>
<idlen2> 62.7 </idlen2>
<maxn1> 105.8 </maxn1>
<maxn2> 102.1</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">
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
</turbine_engine>
