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Add engine components for the Fokker 50

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ehofman 2003-07-27 12:49:41 +00:00
parent 0ba771b580
commit ba21bbf290
2 changed files with 136 additions and 0 deletions
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90
Engine/PW125B_sim.xml Normal file
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<?xml version="1.0"?>
<!--
File: PW125B.xml
Author: Aero-Matic v 0.2
Inputs:
name: PW125B
type: turboprop
power: 2500 hp
augmented? no
injected? no
-->
<FG_SIMTURBINE NAME="PW125B">
MAXMILTHRUST 4175
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>
<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>

46
Engine/propDA-R352_6-123-F_2.xml Normal file
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<xml version="1.0"?>
<!-- Generated by Aero-Matic v 0.3
Inputs:
horsepower: 2500
pitch: variable
Outputs:
linear-blade-inches: 265
-->
<FG_PROPELLER NAME="prop">
IXX 3.7910590942383
DIAMETER 144
NUMBLADES 6
MINPITCH 10
MAXPITCH 30
MINRPM 700
MAXRPM 2700
C_THRUST 11 2
10 30
0.0 0.07488 0.0936
0.1 0.07416 0.0927
0.2 0.07344 0.0918
0.3 0.07272 0.0909
0.4 0.06625 0.0828
0.5 0.05904 0.0738
0.6 0.05040 0.0630
0.7 0.03920 0.0490
0.8 0.02880 0.0360
0.9 0.01600 0.0200
1.0 0.00320 0.0040
C_POWER 11 2
10 30
0.0 0.02287 0.10395
0.1 0.02252 0.10237
0.2 0.02217 0.10080
0.3 0.02148 0.09765
0.4 0.02079 0.09450
0.5 0.02009 0.09135
0.6 0.01905 0.08662
0.7 0.01663 0.07560
0.8 0.01316 0.05985
0.9 0.00866 0.03937
1.0 0.00346 0.01575
</FG_PROPELLER>