2003-07-27 12:49:41 +00:00
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<?xml version="1.0"?>
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<!--
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File: PW125B.xml
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2003-09-06 09:39:22 +00:00
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Author: Aero-Matic v 0.3
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2003-07-27 12:49:41 +00:00
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Inputs:
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name: PW125B
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type: turboprop
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power: 2500 hp
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augmented? no
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injected? no
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-->
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2003-10-19 09:47:23 +00:00
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<!-- 2500 horsepower X 2.24 lbs/hp -->
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2003-07-27 12:49:41 +00:00
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<FG_SIMTURBINE NAME="PW125B">
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2003-10-19 09:47:23 +00:00
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MILTHRUST 5600.00
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MAXTHRUST 5600.00
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2003-07-27 12:49:41 +00:00
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BYPASSRATIO 0.0
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TSFC 0.55
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ATSFC 0.0
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IDLEN1 30.0
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IDLEN2 60.0
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MAXN1 100.0
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MAXN2 100.0
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AUGMENTED 0
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AUGMETHOD 1
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INJECTED 0
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<TABLE NAME="IdleThrust" TYPE="TABLE">
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Idle_power_thrust_factor
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6
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6
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velocities/mach-norm
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position/h-sl-ft
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none
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0 10000 20000 30000 40000 50000
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0.0 0.0836 0.0528 0.0694 0.0899 0.1183 0.1467
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0.2 0.0501 0.0335 0.0544 0.0797 0.1049 0.1342
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0.4 0.0047 0.0020 0.0272 0.0595 0.0891 0.1203
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0.6 0.0 0.0 0.0 0.0276 0.0718 0.1073
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0.8 0.0 0.0 0.0 0.0 0.0474 0.0868
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1.0 0.0 0.0 0.0 0.0 0.0 0.0552
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</TABLE>
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<TABLE NAME="MilThrust" TYPE="TABLE">
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Military_power_thrust_factor
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6
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6
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velocities/mach-norm
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position/h-sl-ft
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none
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0 10000 20000 30000 40000 50000
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0.0 1.0000 0.7400 0.5340 0.3720 0.2410 0.1490
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0.2 0.7340 0.6970 0.5060 0.3550 0.2310 0.1430
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0.4 0.6210 0.5920 0.4060 0.3570 0.2330 0.1450
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0.6 0.3510 0.2710 0.2020 0.1780 0.1020 0.0640
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0.8 0.0200 0.0200 0.0200 0.0200 0.0200 0.0200
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1.0 0.0 0.0 0.0 0.0 0.0 0.0
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</TABLE>
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</FG_SIMTURBINE>
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