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fgdata/Engine/PW125B_sim.xml

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XML

<?xml version="1.0"?>
<!--
File: PW125B.xml
Author: Aero-Matic v 0.3
Inputs:
name: PW125B
type: turboprop
power: 2500 hp
augmented? no
injected? no
-->
<!-- 2500 horsepower X 2.24 lbs/hp -->
<FG_SIMTURBINE NAME="PW125B">
MILTHRUST 5600.00
MAXTHRUST 5600.00
BYPASSRATIO 0.0
TSFC 0.55
ATSFC 0.0
IDLEN1 30.0
IDLEN2 60.0
MAXN1 100.0
MAXN2 100.0
AUGMENTED 0
AUGMETHOD 1
INJECTED 0
<TABLE NAME="IdleThrust" TYPE="TABLE">
Idle_power_thrust_factor
6
6
velocities/mach-norm
position/h-sl-ft
none
0 10000 20000 30000 40000 50000
0.0 0.0836 0.0528 0.0694 0.0899 0.1183 0.1467
0.2 0.0501 0.0335 0.0544 0.0797 0.1049 0.1342
0.4 0.0047 0.0020 0.0272 0.0595 0.0891 0.1203
0.6 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
1.0 0.0 0.0 0.0 0.0 0.0 0.0552
</TABLE>
<TABLE NAME="MilThrust" TYPE="TABLE">
Military_power_thrust_factor
6
6
velocities/mach-norm
position/h-sl-ft
none
0 10000 20000 30000 40000 50000
0.0 1.0000 0.7400 0.5340 0.3720 0.2410 0.1490
0.2 0.7340 0.6970 0.5060 0.3550 0.2310 0.1430
0.4 0.6210 0.5920 0.4060 0.3570 0.2330 0.1450
0.6 0.3510 0.2710 0.2020 0.1780 0.1020 0.0640
0.8 0.0200 0.0200 0.0200 0.0200 0.0200 0.0200
1.0 0.0 0.0 0.0 0.0 0.0 0.0
</TABLE>
</FG_SIMTURBINE>