68 lines
2.1 KiB
XML
68 lines
2.1 KiB
XML
<?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
|
|
2
|
|
2
|
|
velocities/mach-norm
|
|
position/h-sl-ft
|
|
none
|
|
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
|
|
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>
|