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Update the turbine engines to the new layout from David Culp

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This commit is contained in:
ehofman 2003-10-19 09:47:23 +00:00
parent 2f19468e0d
commit a0dac5ae4c
9 changed files with 121 additions and 342 deletions
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42
Engine/CFM56_5_sim.xml
View file

@ -6,7 +6,8 @@
<FG_SIMTURBINE NAME="CFM56_5">
<!--
MAXMILTHRUST max static thrust at S.L. (installed), lbf
MILTHRUST max static thrust at S.L. (installed), lbf
MAXTHRUST max static thrust with afterburner at S.L. (installed), lbf
BYPASSRATIO bypass ratio
TSFC thrust-specific fuel consumption (lbm/hr/lbf)
ATSFC augmented TSFC (lbm/hr/lbf)
@ -23,7 +24,8 @@
TABLE(3) water-injection multiplier vs. altitude and mach
-->
MAXMILTHRUST 25000
MILTHRUST 25000
MAXTHRUST 25000
BYPASSRATIO 5.9
TSFC 0.657
ATSFC 0.0
@ -68,40 +70,4 @@
1.0 0.5000 0.5000 0.4000 0.2000 0.1500 0.0900
</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>

42
Engine/CFM56_sim.xml
View file

@ -6,7 +6,8 @@
<FG_SIMTURBINE NAME="CFM56">
<!--
MAXMILTHRUST max static thrust at S.L. (installed), lbf
MILTHRUST max static thrust (without afterburner) at S.L. (installed), lbf
MAXTHRUST max static thrust with afterburner at S.L. (installed), lbf
BYPASSRATIO bypass ratio
TSFC thrust-specific fuel consumption (lbm/hr/lbf)
ATSFC augmented TSFC (lbm/hr/lbf)
@ -23,7 +24,8 @@
TABLE(3) water-injection multiplier vs. altitude and mach
-->
MAXMILTHRUST 20000
MILTHRUST 20000
MAXTHRUST 20000
BYPASSRATIO 5.9
TSFC 0.657
ATSFC 0.0
@ -68,40 +70,4 @@
1.0 0.5000 0.5000 0.4000 0.2000 0.1500 0.0900
</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>

55
Engine/F100-PW-229_sim.xml
View file

@ -5,7 +5,8 @@
<FG_SIMTURBINE NAME="F100">
<!--
MAXMILTHRUST max static thrust at S.L. (installed), lbf
MILTHRUST max static thrust (without afterburner) at S.L. (installed), lbf
MAXTHRUST max static thrust with afterburner at S.L. (installed), lbf
BYPASSRATIO bypass ratio
TSFC thrust-specific fuel consumption (lbm/hr/lbf)
ATSFC augmented TSFC (lbm/hr/lbf)
@ -24,7 +25,8 @@
TABLE(3) water-injection multiplier vs. altitude and mach
-->
MAXMILTHRUST 17800
MILTHRUST 17800
MAXTHRUST 29000
BYPASSRATIO 0.4
TSFC 0.74
ATSFC 2.05
@ -71,41 +73,30 @@
1.4 1.3400 1.0860 0.8450 0.6280 0.4240 0.2630
</TABLE>
<!-- 29000/17800 = 1.6290 -->
<!-- data from EngineSim, http://www.grc.nasa.gov/WWW/K-12/airplane/ngnsim.html,
extrapolated to higher mach numbers -->
<TABLE NAME="AugThrust" TYPE="TABLE">
Augmented_thrust_factor
8
6
14
7
velocities/mach-norm
position/h-sl-ft
none
0 10000 20000 30000 40000 50000
0.0 1.6290 1.6290 1.6290 1.6290 1.6290 1.6290
0.2 1.6290 1.6290 1.6290 1.6290 1.6290 1.6290
0.4 1.6290 1.6290 1.6290 1.6290 1.6290 1.6290
0.6 1.6290 1.6290 1.6290 1.6290 1.6290 1.6290
0.8 1.6290 1.6290 1.6290 1.6290 1.6290 1.6290
1.0 1.6290 1.6290 1.6290 1.6290 1.6290 1.6290
1.2 1.6290 1.6290 1.6290 1.6290 1.6290 1.6290
1.4 1.6290 1.6290 1.6290 1.6290 1.6290 1.6290
</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
-10000 0 10000 20000 30000 40000 50000
0.0 1.1816 1.0000 0.8184 0.6627 0.5280 0.3756 0.2327
0.2 1.1308 0.9599 0.7890 0.6406 0.5116 0.3645 0.2258
0.4 1.1150 0.9474 0.7798 0.6340 0.5070 0.3615 0.2240
0.6 1.1284 0.9589 0.7894 0.6420 0.5134 0.3661 0.2268
0.8 1.1707 0.9942 0.8177 0.6647 0.5309 0.3784 0.2345
1.0 1.2411 1.0529 0.8648 0.7017 0.5596 0.3983 0.2467
1.2 1.3287 1.1254 0.9221 0.7462 0.5936 0.4219 0.2614
1.4 1.4365 1.2149 0.9933 0.8021 0.6360 0.4509 0.2794
1.6 1.5711 1.3260 1.0809 0.8700 0.6874 0.4860 0.3011
1.8 1.7301 1.4579 1.1857 0.9512 0.7495 0.5289 0.3277
2.0 1.8314 1.5700 1.3086 1.0474 0.8216 0.5786 0.3585
2.2 1.9700 1.6900 1.4100 1.2400 0.9100 0.6359 0.3940
2.4 2.0700 1.8000 1.5300 1.3400 1.0000 0.7200 0.4600
2.6 2.2000 1.9200 1.6400 1.4400 1.1000 0.8000 0.5200
</TABLE>
</FG_SIMTURBINE>

85
Engine/J85-GE-5_sim.xml
View file

@ -5,15 +5,16 @@
<FG_SIMTURBINE NAME="J85">
<!--
MAXMILTHRUST max static thrust at S.L. (installed), lbf
MILTHRUST max static thrust at S.L. (installed), lbf
MAXTHRUST max static thrust at S.L. (installed) with afterburning, lbf
BYPASSRATIO bypass ratio
TSFC thrust-specific fuel consumption (lbm/hr/lbf)
ATSFC augmented TSFC (lbm/hr/lbf)
ATSFC afterburning 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
AUGMENTED = 1 if afterburning 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
@ -24,10 +25,11 @@
TABLE(3) water-injection multiplier vs. altitude and mach
-->
MAXMILTHRUST 2050
MILTHRUST 2050
MAXTHRUST 2900
BYPASSRATIO 0
TSFC 0.85
ATSFC 1.70
ATSFC 1.72
IDLEN1 0.0
IDLEN2 53.0
MAXN1 100.0
@ -39,72 +41,67 @@
<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 0.1341
0.4 0.0047 0.0020 0.0272 0.0595 0.0891 0.1203
0.6 -0.0804 -0.0560 -0.0237 0.0276 0.0718 0.1073
0.8 -0.2129 -0.1498 -0.1025 -0.0195 0.0473 0.0868
1.0 -0.2839 -0.1104 -0.0469 -0.0270 -0.0158 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 0.1341
0.4 0.0040 0.0047 0.0020 0.0272 0.0595 0.0891 0.1203
0.6 -0.0900 -0.0804 -0.0560 -0.0237 0.0276 0.0718 0.1073
0.8 -0.2200 -0.2129 -0.1498 -0.1025 -0.0195 0.0473 0.0868
1.0 -0.3000 -0.2839 -0.1104 -0.0469 -0.0270 -0.0158 0.0552
</TABLE>
<!-- data from EngineSim, http://www.grc.nasa.gov/WWW/K-12/airplane/ngnsim.html -->
<TABLE NAME="MilThrust" TYPE="TABLE">
Military_power_thrust_factor
8
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 0.9340 0.6970 0.5060 0.3550 0.2310 0.1430
0.4 0.9210 0.6920 0.5060 0.3570 0.2330 0.1450
0.6 0.9510 0.7210 0.5320 0.3780 0.2480 0.1540
0.8 1.0200 0.7820 0.5820 0.4170 0.2750 0.1700
1.0 1.1200 0.8710 0.6510 0.4750 0.3150 0.1950
1.2 1.2300 0.9750 0.7440 0.5450 0.3640 0.2250
1.4 1.3400 1.0860 0.8450 0.6280 0.4240 0.2630
-10000 0 10000 20000 30000 40000 50000
0.0 1.2600 1.0000 0.7400 0.5340 0.3720 0.2410 0.1490
0.2 1.1710 0.9340 0.6970 0.5060 0.3550 0.2310 0.1430
0.4 1.1500 0.9210 0.6920 0.5060 0.3570 0.2330 0.1450
0.6 1.1810 0.9510 0.7210 0.5320 0.3780 0.2480 0.1540
0.8 1.2580 1.0200 0.7820 0.5820 0.4170 0.2750 0.1700
1.0 1.3690 1.1200 0.8710 0.6510 0.4750 0.3150 0.1950
1.2 1.4850 1.2300 0.9750 0.7440 0.5450 0.3640 0.2250
1.4 1.5940 1.3400 1.0860 0.8450 0.6280 0.4240 0.2630
</TABLE>
<!-- data from EngineSim, http://www.grc.nasa.gov/WWW/K-12/airplane/ngnsim.html -->
<TABLE NAME="AugThrust" TYPE="TABLE">
Augmented_thrust_factor
8
6
7
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
-10000 0 10000 20000 30000 40000 50000
0.0 1.1816 1.0000 0.8184 0.6627 0.5280 0.3756 0.2327
0.2 1.1308 0.9599 0.7890 0.6406 0.5116 0.3645 0.2258
0.4 1.1150 0.9474 0.7798 0.6340 0.5070 0.3615 0.2240
0.6 1.1284 0.9589 0.7894 0.6420 0.5134 0.3661 0.2268
0.8 1.1707 0.9942 0.8177 0.6647 0.5309 0.3784 0.2345
1.0 1.2411 1.0529 0.8648 0.7017 0.5596 0.3983 0.2467
1.2 1.3287 1.1254 0.9221 0.7462 0.5936 0.4219 0.2614
1.4 1.4365 1.2149 0.9933 0.8021 0.6360 0.4509 0.2794
</TABLE>
<TABLE NAME="WaterFactor" TYPE="TABLE">
Water_Injection_factor
8
6
2
2
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
0 50000
0.0 1.2000 1.2000
1.4 1.2000 1.2000
</TABLE>
</FG_SIMTURBINE>

77
Engine/PT6A-68_sim.xml
View file

@ -5,7 +5,8 @@
<FG_SIMTURBINE NAME="PT6A-68">
<!--
MAXMILTHRUST max static thrust at S.L. (installed), lbf
MILTHRUST max static thrust 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)
@ -23,8 +24,9 @@
TABLE(2) augmented thrust multiplier vs. altitude and mach
TABLE(3) water-injection multiplier vs. altitude and mach
-->
MAXMILTHRUST 1500
<!-- 1100 horsepower X 2.24 lb/hp -->
MILTHRUST 2464
MAXTHRUST 2464
BYPASSRATIO 0
TSFC 0.55
ATSFC 0.00
@ -52,59 +54,20 @@
1.0 -0.2839 -0.1104 -0.0469 -0.0270 -0.0158 0.0552
</TABLE>
<!-- data from EngineSim, http://www.grc.nasa.gov/WWW/K-12/airplane/ngnsim.html -->
<TABLE NAME="MilThrust" TYPE="TABLE">
Military_power_thrust_factor
8
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 0.9340 0.6970 0.5060 0.3550 0.2310 0.1430
0.4 0.9210 0.6920 0.5060 0.3570 0.2330 0.1450
0.6 0.9510 0.7210 0.5320 0.3780 0.2480 0.1540
0.8 1.0200 0.7820 0.5820 0.4170 0.2750 0.1700
1.0 1.1200 0.8710 0.6510 0.4750 0.3150 0.1950
1.2 1.2300 0.9750 0.7440 0.5450 0.3640 0.2250
1.4 1.3400 1.0860 0.8450 0.6280 0.4240 0.2630
</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>
<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>

39
Engine/PW125B_sim.xml
View file

@ -10,9 +10,10 @@
augmented? no
injected? no
-->
<!-- 2500 horsepower X 2.24 lbs/hp -->
<FG_SIMTURBINE NAME="PW125B">
MAXMILTHRUST 4175.00
MILTHRUST 5600.00
MAXTHRUST 5600.00
BYPASSRATIO 0.0
TSFC 0.55
ATSFC 0.0
@ -53,38 +54,4 @@
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>

76
Engine/T76_sim.xml
View file

@ -5,7 +5,8 @@
<FG_SIMTURBINE NAME="T76">
<!--
MAXMILTHRUST max static thrust at S.L. (installed), lbf
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)
@ -24,7 +25,8 @@
TABLE(3) water-injection multiplier vs. altitude and mach
-->
MAXMILTHRUST 1200
MILTHRUST 1600
MAXTHRUST 1600
BYPASSRATIO 0
TSFC 0.55
ATSFC 0.00
@ -52,59 +54,19 @@
1.0 -0.2839 -0.1104 -0.0469 -0.0270 -0.0158 0.0552
</TABLE>
<!-- data from EngineSim, http://www.grc.nasa.gov/WWW/K-12/airplane/ngnsim.html -->
<TABLE NAME="MilThrust" TYPE="TABLE">
Military_power_thrust_factor
8
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 0.9340 0.6970 0.5060 0.3550 0.2310 0.1430
0.4 0.9210 0.6920 0.5060 0.3570 0.2330 0.1450
0.6 0.9510 0.7210 0.5320 0.3780 0.2480 0.1540
0.8 1.0200 0.7820 0.5820 0.4170 0.2750 0.1700
1.0 1.1200 0.8710 0.6510 0.4750 0.3150 0.1950
1.2 1.2300 0.9750 0.7440 0.5450 0.3640 0.2250
1.4 1.3400 1.0860 0.8450 0.6280 0.4240 0.2630
</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>
<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>

37
Engine/Tay-651_sim.xml
View file

@ -12,7 +12,8 @@
-->
<FG_SIMTURBINE NAME="Tay-650">
MAXMILTHRUST 15400
MILTHRUST 15400
MAXTHRUST 15400
BYPASSRATIO 1.0
TSFC 0.8
ATSFC 1.7
@ -55,38 +56,4 @@
1.2 1.2300 0.9750 0.7440 0.5450 0.3640 0.2250
1.4 1.3400 1.0860 0.8450 0.6280 0.4240 0.2630
</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>

10
Engine/propDA-R352_6-123-F_2.xml
View file

@ -1,18 +1,18 @@
<xml version="1.0"?>
<!-- Generated by Aero-Matic v 0.3
<!-- Generated by Aero-Matic v 0.7
Inputs:
horsepower: 2500
horsepower: 2250
pitch: variable
Outputs:
linear-blade-inches: 265
linear-blade-inches: 251.40107398339
-->
<FG_PROPELLER NAME="prop">
IXX 3.7910590942383
DIAMETER 144
NUMBLADES 6
DIAMETER 75
NUMBLADES 4
MINPITCH 10
MAXPITCH 30
MINRPM 700