This repository has been archived on 2021-09-26. You can view files and clone it, but cannot push or open issues or pull requests.
IDG-A32X/Engines/v2522_a5.xml

63 lines
2.2 KiB
XML
Raw Normal View History

2016-11-07 15:39:53 +00:00
<?xml version="1.0"?>
<!--
File: V2522_A5.xml
Author: Aero-Matic v 0.81
Inputs:
name: V2522_A5
type: turbine
thrust: 23000 lb
2016-11-07 15:39:53 +00:00
augmented? no
injected? no
-->
<turbine_engine name="V2527_A5">
<milthrust> 23000 </milthrust>
2017-05-16 13:39:49 +00:00
<bypassratio> 8.1 </bypassratio>
2016-11-07 15:39:53 +00:00
<tsfc> 0.8 </tsfc>
<bleed> 0.03 </bleed>
2016-11-07 15:39:53 +00:00
<idlen1> 23.4 </idlen1>
<idlen2> 63.7 </idlen2>
<n1spinup> 0.2 </n1spinup>
<n2spinup> 2.0 </n2spinup>
2016-11-07 15:39:53 +00:00
<maxn1> 105.8 </maxn1>
2017-01-11 22:39:47 +00:00
<maxn2> 102.1 </maxn2>
2016-11-07 15:39:53 +00:00
<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>