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fgdata/Engine/T76_sim.xml

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<?xml version="1.0"?>
<!-- T76 turboprop engine model
for the SimTurbine turbine model -->
<FG_SIMTURBINE NAME="T76">
<!--
MILTHRUST max static thrust (without afterburning) at S.L. (installed), lbf
MAXTHRUST max static thrust with afterburning at S.L. (installed), lbf
BYPASSRATIO bypass ratio
TSFC thrust-specific fuel consumption (lbm/hr/lbf)
ATSFC augmented TSFC (lbm/hr/lbf)
IDLEN1 idle percent rpm of fan spool
IDLEN2 idle percent rpm of inner spool
MAXN1 N1 at 100% throttle
MAXN2 N2 at 100% throttle
AUGMENTED = 1 if augmentation installed, else = 0
AUGMETHOD = 0 if using property /engine[n]/augmentation
= 1 if using last 1% of throttle movement
INJECTED = 1 if water injection installed
TABLE(0) idle thrust vs. altitude and mach
TABLE(1) maximum un-augmented thrust vs. altitude and mach
TABLE(2) augmented thrust multiplier vs. altitude and mach
TABLE(3) water-injection multiplier vs. altitude and mach
-->
MILTHRUST 1600
MAXTHRUST 1600
BYPASSRATIO 0
TSFC 0.55
ATSFC 0.00
IDLEN1 0.0
IDLEN2 61.0
MAXN1 0.0
MAXN2 100.0
AUGMENTED 0
AUGMETHOD 0
INJECTED 0
<TABLE NAME="IdleThrust" TYPE="TABLE">
Idle_power_thrust_factor
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2
2
velocities/mach-norm
position/h-sl-ft
none
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0 40000
0.0 0.0000 0.0000
1.0 0.0000 0.0000
</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
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0.6 0.3210 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>