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Updates to match the Fokker 50

This commit is contained in:
ehofman 2004-04-10 13:55:56 +00:00
parent e4fd2a455a
commit a73075dc12

View file

@ -1,19 +1,19 @@
<?xml version="1.0"?>
<!--
File: PW125B.xml
Author: Aero-Matic v 0.3
File: PW172B.xml
Author: Aero-Matic v 0.7
Inputs:
name: PW125B
name: PW172B
type: turboprop
power: 2500 hp
power: 2750 hp
augmented? no
injected? no
-->
<!-- 2500 horsepower X 2.24 lbs/hp -->
<FG_SIMTURBINE NAME="PW125B">
MILTHRUST 5600.00
MAXTHRUST 5600.00
<FG_SIMTURBINE NAME="PW172B">
MILTHRUST 6160.00
MAXTHRUST 6160.00
BYPASSRATIO 0.0
TSFC 0.55
ATSFC 0.0
@ -24,34 +24,37 @@
AUGMENTED 0
AUGMETHOD 1
INJECTED 0
<TABLE NAME="IdleThrust" TYPE="TABLE">
Idle_power_thrust_factor
6
6
7
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
-10000 0 10000 20000 30000 40000 50000
0.0 0.0430 0.0488 0.0528 0.0694 0.0899 0.1183 0.1467
0.2 0.0500 0.0501 0.0335 0.0544 0.0797 0.1049 0.1342
0.4 0.0040 0.0047 0.0020 0.0272 0.0595 0.0891 0.1203
0.6 0.0 0.0 0.0 0.0276 0.0718 0.0430 0.0
0.8 0.0 0.0 0.0 0.0 0.0174 0.0086 0.0
1.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0
</TABLE>
<TABLE NAME="MilThrust" TYPE="TABLE">
Military_power_thrust_factor
6
6
7
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
-10000 0 10000 20000 30000 40000 50000
0.0 1.1260 1.0000 0.7400 0.5340 0.3720 0.2410 0.1490
0.2 1.1000 0.9340 0.6970 0.5060 0.3550 0.2310 0.1430
0.4 1.0000 0.6410 0.6120 0.4060 0.3570 0.2330 0.1450
0.6 0.4430 0.3510 0.2710 0.2020 0.1780 0.1020 0.0640
0.8 0.0240 0.0200 0.0160 0.0130 0.0110 0.0100 0.0
1.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0
</TABLE>
</FG_SIMTURBINE>