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fgdata/Engine/Tay-651_sim.xml

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XML

<?xml version="1.0"?>
<!--
File: Tay-650.xml
Author: Aero-Matic v 0.2
Inputs:
name: Tay-650
type: turbine
thrust: 15400 lb
augmented? no
injected? no
-->
<FG_SIMTURBINE NAME="Tay-650">
MAXMILTHRUST 15400
BYPASSRATIO 1.0
TSFC 0.8
ATSFC 1.7
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
8
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 0.9340 0.6970 0.5060 0.3550 0.2310 0.1430
0.4 0.9210 0.6920 0.5060 0.3570 0.2330 0.1450
0.6 0.9510 0.7210 0.5320 0.3780 0.2480 0.1540
0.8 1.0200 0.7820 0.5820 0.4170 0.2750 0.1700
1.0 1.1200 0.8710 0.6510 0.4750 0.3150 0.1950
1.2 1.2300 0.9750 0.7440 0.5450 0.3640 0.2250
1.4 1.3400 1.0860 0.8450 0.6280 0.4240 0.2630
</TABLE>
<TABLE NAME="AugThrust" TYPE="TABLE">
Augmented_thrust_factor
8
6
velocities/mach-norm
position/h-sl-ft
none
0 10000 20000 30000 40000 50000
0.0 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
0.2 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
0.4 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
0.6 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
0.8 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
1.0 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
1.2 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
1.4 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
</TABLE>
<TABLE NAME="WaterFactor" TYPE="TABLE">
Water_injection_factor
8
6
velocities/mach-norm
position/h-sl-ft
none
0 10000 20000 30000 40000 50000
0.0 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
0.2 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
0.4 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
0.6 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
0.8 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
1.0 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
1.2 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
1.4 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
</TABLE>
</FG_SIMTURBINE>