57 lines
1.6 KiB
XML
57 lines
1.6 KiB
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>
|