Update the turbine engines to the new layout from David Culp
This commit is contained in:
ehofman
parent
2f19468e0d
commit
a0dac5ae4c
9 changed files with 121 additions and 342 deletions
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@ -6,7 +6,8 @@
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<FG_SIMTURBINE NAME="CFM56_5">
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<FG_SIMTURBINE NAME="CFM56_5">
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<!--
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<!--
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MAXMILTHRUST max static thrust at S.L. (installed), lbf
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MILTHRUST max static thrust at S.L. (installed), lbf
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MAXTHRUST max static thrust with afterburner at S.L. (installed), lbf
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BYPASSRATIO bypass ratio
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BYPASSRATIO bypass ratio
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TSFC thrust-specific fuel consumption (lbm/hr/lbf)
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TSFC thrust-specific fuel consumption (lbm/hr/lbf)
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ATSFC augmented TSFC (lbm/hr/lbf)
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ATSFC augmented TSFC (lbm/hr/lbf)
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@ -23,7 +24,8 @@
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TABLE(3) water-injection multiplier vs. altitude and mach
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TABLE(3) water-injection multiplier vs. altitude and mach
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-->
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-->
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MAXMILTHRUST 25000
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MILTHRUST 25000
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MAXTHRUST 25000
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BYPASSRATIO 5.9
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BYPASSRATIO 5.9
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TSFC 0.657
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TSFC 0.657
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ATSFC 0.0
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ATSFC 0.0
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@ -68,40 +70,4 @@
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1.0 0.5000 0.5000 0.4000 0.2000 0.1500 0.0900
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1.0 0.5000 0.5000 0.4000 0.2000 0.1500 0.0900
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</TABLE>
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</TABLE>
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<TABLE NAME="AugThrust" TYPE="TABLE">
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Augmented_thrust_factor
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8
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6
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velocities/mach-norm
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position/h-sl-ft
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none
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0 10000 20000 30000 40000 50000
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0.0 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
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0.2 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
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0.4 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
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0.6 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
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0.8 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
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1.0 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
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1.2 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
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1.4 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
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</TABLE>
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<TABLE NAME="WaterFactor" TYPE="TABLE">
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Water_Injection_factor
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8
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6
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velocities/mach-norm
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position/h-sl-ft
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none
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0 10000 20000 30000 40000 50000
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0.0 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
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0.2 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
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0.4 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
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0.6 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
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0.8 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
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1.0 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
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1.2 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
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1.4 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
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</TABLE>
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</FG_SIMTURBINE>
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</FG_SIMTURBINE>
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@ -6,7 +6,8 @@
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<FG_SIMTURBINE NAME="CFM56">
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<FG_SIMTURBINE NAME="CFM56">
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<!--
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<!--
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MAXMILTHRUST max static thrust at S.L. (installed), lbf
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MILTHRUST max static thrust (without afterburner) at S.L. (installed), lbf
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MAXTHRUST max static thrust with afterburner at S.L. (installed), lbf
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BYPASSRATIO bypass ratio
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BYPASSRATIO bypass ratio
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TSFC thrust-specific fuel consumption (lbm/hr/lbf)
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TSFC thrust-specific fuel consumption (lbm/hr/lbf)
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ATSFC augmented TSFC (lbm/hr/lbf)
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ATSFC augmented TSFC (lbm/hr/lbf)
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@ -23,7 +24,8 @@
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TABLE(3) water-injection multiplier vs. altitude and mach
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TABLE(3) water-injection multiplier vs. altitude and mach
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-->
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-->
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MAXMILTHRUST 20000
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MILTHRUST 20000
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MAXTHRUST 20000
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BYPASSRATIO 5.9
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BYPASSRATIO 5.9
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TSFC 0.657
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TSFC 0.657
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ATSFC 0.0
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ATSFC 0.0
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@ -68,40 +70,4 @@
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1.0 0.5000 0.5000 0.4000 0.2000 0.1500 0.0900
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1.0 0.5000 0.5000 0.4000 0.2000 0.1500 0.0900
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</TABLE>
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</TABLE>
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<TABLE NAME="AugThrust" TYPE="TABLE">
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Augmented_thrust_factor
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8
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6
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velocities/mach-norm
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position/h-sl-ft
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none
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0 10000 20000 30000 40000 50000
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0.0 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
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0.2 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
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0.4 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
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0.6 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
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0.8 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
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1.0 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
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1.2 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
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1.4 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
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</TABLE>
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<TABLE NAME="WaterFactor" TYPE="TABLE">
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Water_Injection_factor
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8
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6
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velocities/mach-norm
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position/h-sl-ft
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none
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0 10000 20000 30000 40000 50000
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0.0 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
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0.2 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
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0.4 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
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0.6 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
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0.8 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
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1.0 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
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1.2 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
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1.4 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
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</TABLE>
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</FG_SIMTURBINE>
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</FG_SIMTURBINE>
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@ -5,7 +5,8 @@
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<FG_SIMTURBINE NAME="F100">
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<FG_SIMTURBINE NAME="F100">
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<!--
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<!--
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MAXMILTHRUST max static thrust at S.L. (installed), lbf
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MILTHRUST max static thrust (without afterburner) at S.L. (installed), lbf
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MAXTHRUST max static thrust with afterburner at S.L. (installed), lbf
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BYPASSRATIO bypass ratio
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BYPASSRATIO bypass ratio
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TSFC thrust-specific fuel consumption (lbm/hr/lbf)
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TSFC thrust-specific fuel consumption (lbm/hr/lbf)
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ATSFC augmented TSFC (lbm/hr/lbf)
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ATSFC augmented TSFC (lbm/hr/lbf)
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@ -24,7 +25,8 @@
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TABLE(3) water-injection multiplier vs. altitude and mach
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TABLE(3) water-injection multiplier vs. altitude and mach
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-->
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-->
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MAXMILTHRUST 17800
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MILTHRUST 17800
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MAXTHRUST 29000
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BYPASSRATIO 0.4
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BYPASSRATIO 0.4
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TSFC 0.74
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TSFC 0.74
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ATSFC 2.05
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ATSFC 2.05
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@ -71,41 +73,30 @@
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1.4 1.3400 1.0860 0.8450 0.6280 0.4240 0.2630
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1.4 1.3400 1.0860 0.8450 0.6280 0.4240 0.2630
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</TABLE>
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</TABLE>
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<!-- 29000/17800 = 1.6290 -->
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<!-- data from EngineSim, http://www.grc.nasa.gov/WWW/K-12/airplane/ngnsim.html,
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extrapolated to higher mach numbers -->
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<TABLE NAME="AugThrust" TYPE="TABLE">
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<TABLE NAME="AugThrust" TYPE="TABLE">
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Augmented_thrust_factor
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Augmented_thrust_factor
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8
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14
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6
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7
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velocities/mach-norm
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velocities/mach-norm
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position/h-sl-ft
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position/h-sl-ft
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none
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none
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0 10000 20000 30000 40000 50000
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-10000 0 10000 20000 30000 40000 50000
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0.0 1.6290 1.6290 1.6290 1.6290 1.6290 1.6290
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0.0 1.1816 1.0000 0.8184 0.6627 0.5280 0.3756 0.2327
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0.2 1.6290 1.6290 1.6290 1.6290 1.6290 1.6290
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0.2 1.1308 0.9599 0.7890 0.6406 0.5116 0.3645 0.2258
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0.4 1.6290 1.6290 1.6290 1.6290 1.6290 1.6290
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0.4 1.1150 0.9474 0.7798 0.6340 0.5070 0.3615 0.2240
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0.6 1.6290 1.6290 1.6290 1.6290 1.6290 1.6290
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0.6 1.1284 0.9589 0.7894 0.6420 0.5134 0.3661 0.2268
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0.8 1.6290 1.6290 1.6290 1.6290 1.6290 1.6290
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0.8 1.1707 0.9942 0.8177 0.6647 0.5309 0.3784 0.2345
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1.0 1.6290 1.6290 1.6290 1.6290 1.6290 1.6290
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1.0 1.2411 1.0529 0.8648 0.7017 0.5596 0.3983 0.2467
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1.2 1.6290 1.6290 1.6290 1.6290 1.6290 1.6290
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1.2 1.3287 1.1254 0.9221 0.7462 0.5936 0.4219 0.2614
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1.4 1.6290 1.6290 1.6290 1.6290 1.6290 1.6290
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1.4 1.4365 1.2149 0.9933 0.8021 0.6360 0.4509 0.2794
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</TABLE>
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1.6 1.5711 1.3260 1.0809 0.8700 0.6874 0.4860 0.3011
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1.8 1.7301 1.4579 1.1857 0.9512 0.7495 0.5289 0.3277
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<TABLE NAME="WaterFactor" TYPE="TABLE">
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2.0 1.8314 1.5700 1.3086 1.0474 0.8216 0.5786 0.3585
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Water_Injection_factor
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2.2 1.9700 1.6900 1.4100 1.2400 0.9100 0.6359 0.3940
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8
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2.4 2.0700 1.8000 1.5300 1.3400 1.0000 0.7200 0.4600
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6
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2.6 2.2000 1.9200 1.6400 1.4400 1.1000 0.8000 0.5200
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velocities/mach-norm
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position/h-sl-ft
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none
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0 10000 20000 30000 40000 50000
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0.0 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
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0.2 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
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0.4 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
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0.6 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
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0.8 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
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1.0 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
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1.2 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
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1.4 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
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</TABLE>
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</TABLE>
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</FG_SIMTURBINE>
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</FG_SIMTURBINE>
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<FG_SIMTURBINE NAME="J85">
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<FG_SIMTURBINE NAME="J85">
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<!--
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<!--
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MAXMILTHRUST max static thrust at S.L. (installed), lbf
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MILTHRUST max static thrust at S.L. (installed), lbf
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MAXTHRUST max static thrust at S.L. (installed) with afterburning, lbf
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BYPASSRATIO bypass ratio
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BYPASSRATIO bypass ratio
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TSFC thrust-specific fuel consumption (lbm/hr/lbf)
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TSFC thrust-specific fuel consumption (lbm/hr/lbf)
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ATSFC augmented TSFC (lbm/hr/lbf)
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ATSFC afterburning TSFC (lbm/hr/lbf)
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IDLEN1 idle percent rpm of fan spool
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IDLEN1 idle percent rpm of fan spool
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IDLEN2 idle percent rpm of inner spool
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IDLEN2 idle percent rpm of inner spool
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MAXN1 N1 at 100% throttle
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MAXN1 N1 at 100% throttle
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MAXN2 N2 at 100% throttle
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MAXN2 N2 at 100% throttle
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AUGMENTED = 1 if augmentation installed, else = 0
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AUGMENTED = 1 if afterburning installed, else = 0
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AUGMETHOD = 0 if using property /engine[n]/augmentation
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AUGMETHOD = 0 if using property /engine[n]/augmentation
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= 1 if using last 1% of throttle movement
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= 1 if using last 1% of throttle movement
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INJECTED = 1 if water injection installed
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INJECTED = 1 if water injection installed
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TABLE(3) water-injection multiplier vs. altitude and mach
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TABLE(3) water-injection multiplier vs. altitude and mach
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-->
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-->
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MAXMILTHRUST 2050
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MILTHRUST 2050
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MAXTHRUST 2900
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BYPASSRATIO 0
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BYPASSRATIO 0
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TSFC 0.85
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TSFC 0.85
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ATSFC 1.70
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ATSFC 1.72
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IDLEN1 0.0
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IDLEN1 0.0
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IDLEN2 53.0
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IDLEN2 53.0
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MAXN1 100.0
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MAXN1 100.0
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<TABLE NAME="IdleThrust" TYPE="TABLE">
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<TABLE NAME="IdleThrust" TYPE="TABLE">
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Idle_power_thrust_factor
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Idle_power_thrust_factor
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6
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6
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6
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7
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velocities/mach-norm
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velocities/mach-norm
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position/h-sl-ft
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position/h-sl-ft
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none
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none
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0 10000 20000 30000 40000 50000
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-10000 0 10000 20000 30000 40000 50000
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0.0 0.0836 0.0528 0.0694 0.0899 0.1183 0.1467
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0.0 0.0430 0.0488 0.0528 0.0694 0.0899 0.1183 0.1467
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0.2 0.0501 0.0335 0.0544 0.0797 0.1049 0.1341
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0.2 0.0500 0.0501 0.0335 0.0544 0.0797 0.1049 0.1341
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0.4 0.0047 0.0020 0.0272 0.0595 0.0891 0.1203
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0.4 0.0040 0.0047 0.0020 0.0272 0.0595 0.0891 0.1203
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0.6 -0.0804 -0.0560 -0.0237 0.0276 0.0718 0.1073
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0.6 -0.0900 -0.0804 -0.0560 -0.0237 0.0276 0.0718 0.1073
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0.8 -0.2129 -0.1498 -0.1025 -0.0195 0.0473 0.0868
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0.8 -0.2200 -0.2129 -0.1498 -0.1025 -0.0195 0.0473 0.0868
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1.0 -0.2839 -0.1104 -0.0469 -0.0270 -0.0158 0.0552
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1.0 -0.3000 -0.2839 -0.1104 -0.0469 -0.0270 -0.0158 0.0552
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</TABLE>
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</TABLE>
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<!-- data from EngineSim, http://www.grc.nasa.gov/WWW/K-12/airplane/ngnsim.html -->
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<!-- data from EngineSim, http://www.grc.nasa.gov/WWW/K-12/airplane/ngnsim.html -->
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<TABLE NAME="MilThrust" TYPE="TABLE">
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<TABLE NAME="MilThrust" TYPE="TABLE">
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Military_power_thrust_factor
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Military_power_thrust_factor
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8
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8
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6
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7
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velocities/mach-norm
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velocities/mach-norm
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position/h-sl-ft
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position/h-sl-ft
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none
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none
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0 10000 20000 30000 40000 50000
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-10000 0 10000 20000 30000 40000 50000
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0.0 1.0000 0.7400 0.5340 0.3720 0.2410 0.1490
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0.0 1.2600 1.0000 0.7400 0.5340 0.3720 0.2410 0.1490
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0.2 0.9340 0.6970 0.5060 0.3550 0.2310 0.1430
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0.2 1.1710 0.9340 0.6970 0.5060 0.3550 0.2310 0.1430
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0.4 0.9210 0.6920 0.5060 0.3570 0.2330 0.1450
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0.4 1.1500 0.9210 0.6920 0.5060 0.3570 0.2330 0.1450
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0.6 0.9510 0.7210 0.5320 0.3780 0.2480 0.1540
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0.6 1.1810 0.9510 0.7210 0.5320 0.3780 0.2480 0.1540
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0.8 1.0200 0.7820 0.5820 0.4170 0.2750 0.1700
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0.8 1.2580 1.0200 0.7820 0.5820 0.4170 0.2750 0.1700
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1.0 1.1200 0.8710 0.6510 0.4750 0.3150 0.1950
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1.0 1.3690 1.1200 0.8710 0.6510 0.4750 0.3150 0.1950
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1.2 1.2300 0.9750 0.7440 0.5450 0.3640 0.2250
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1.2 1.4850 1.2300 0.9750 0.7440 0.5450 0.3640 0.2250
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1.4 1.3400 1.0860 0.8450 0.6280 0.4240 0.2630
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1.4 1.5940 1.3400 1.0860 0.8450 0.6280 0.4240 0.2630
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</TABLE>
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</TABLE>
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||||||
|
<!-- data from EngineSim, http://www.grc.nasa.gov/WWW/K-12/airplane/ngnsim.html -->
|
||||||
<TABLE NAME="AugThrust" TYPE="TABLE">
|
<TABLE NAME="AugThrust" TYPE="TABLE">
|
||||||
Augmented_thrust_factor
|
Augmented_thrust_factor
|
||||||
8
|
8
|
||||||
6
|
7
|
||||||
velocities/mach-norm
|
velocities/mach-norm
|
||||||
position/h-sl-ft
|
position/h-sl-ft
|
||||||
none
|
none
|
||||||
0 10000 20000 30000 40000 50000
|
-10000 0 10000 20000 30000 40000 50000
|
||||||
0.0 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
|
0.0 1.1816 1.0000 0.8184 0.6627 0.5280 0.3756 0.2327
|
||||||
0.2 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
|
0.2 1.1308 0.9599 0.7890 0.6406 0.5116 0.3645 0.2258
|
||||||
0.4 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
|
0.4 1.1150 0.9474 0.7798 0.6340 0.5070 0.3615 0.2240
|
||||||
0.6 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
|
0.6 1.1284 0.9589 0.7894 0.6420 0.5134 0.3661 0.2268
|
||||||
0.8 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
|
0.8 1.1707 0.9942 0.8177 0.6647 0.5309 0.3784 0.2345
|
||||||
1.0 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
|
1.0 1.2411 1.0529 0.8648 0.7017 0.5596 0.3983 0.2467
|
||||||
1.2 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
|
1.2 1.3287 1.1254 0.9221 0.7462 0.5936 0.4219 0.2614
|
||||||
1.4 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
|
1.4 1.4365 1.2149 0.9933 0.8021 0.6360 0.4509 0.2794
|
||||||
</TABLE>
|
</TABLE>
|
||||||
|
|
||||||
<TABLE NAME="WaterFactor" TYPE="TABLE">
|
<TABLE NAME="WaterFactor" TYPE="TABLE">
|
||||||
Water_Injection_factor
|
Water_Injection_factor
|
||||||
8
|
2
|
||||||
6
|
2
|
||||||
velocities/mach-norm
|
velocities/mach-norm
|
||||||
position/h-sl-ft
|
position/h-sl-ft
|
||||||
none
|
none
|
||||||
0 10000 20000 30000 40000 50000
|
0 50000
|
||||||
0.0 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
|
0.0 1.2000 1.2000
|
||||||
0.2 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
|
1.4 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>
|
||||||
|
|
||||||
</FG_SIMTURBINE>
|
</FG_SIMTURBINE>
|
||||||
|
|
|
||||||
|
|
@ -5,7 +5,8 @@
|
||||||
|
|
||||||
<FG_SIMTURBINE NAME="PT6A-68">
|
<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
|
BYPASSRATIO bypass ratio
|
||||||
TSFC thrust-specific fuel consumption (lbm/hr/lbf)
|
TSFC thrust-specific fuel consumption (lbm/hr/lbf)
|
||||||
ATSFC augmented TSFC (lbm/hr/lbf)
|
ATSFC augmented TSFC (lbm/hr/lbf)
|
||||||
|
|
@ -23,8 +24,9 @@
|
||||||
TABLE(2) augmented thrust multiplier vs. altitude and mach
|
TABLE(2) augmented thrust multiplier vs. altitude and mach
|
||||||
TABLE(3) water-injection multiplier vs. altitude and mach
|
TABLE(3) water-injection multiplier vs. altitude and mach
|
||||||
-->
|
-->
|
||||||
|
<!-- 1100 horsepower X 2.24 lb/hp -->
|
||||||
MAXMILTHRUST 1500
|
MILTHRUST 2464
|
||||||
|
MAXTHRUST 2464
|
||||||
BYPASSRATIO 0
|
BYPASSRATIO 0
|
||||||
TSFC 0.55
|
TSFC 0.55
|
||||||
ATSFC 0.00
|
ATSFC 0.00
|
||||||
|
|
@ -52,59 +54,20 @@
|
||||||
1.0 -0.2839 -0.1104 -0.0469 -0.0270 -0.0158 0.0552
|
1.0 -0.2839 -0.1104 -0.0469 -0.0270 -0.0158 0.0552
|
||||||
</TABLE>
|
</TABLE>
|
||||||
|
|
||||||
<!-- data from EngineSim, http://www.grc.nasa.gov/WWW/K-12/airplane/ngnsim.html -->
|
<TABLE NAME="MilThrust" TYPE="TABLE">
|
||||||
<TABLE NAME="MilThrust" TYPE="TABLE">
|
Military_power_thrust_factor
|
||||||
Military_power_thrust_factor
|
6
|
||||||
8
|
6
|
||||||
6
|
velocities/mach-norm
|
||||||
velocities/mach-norm
|
position/h-sl-ft
|
||||||
position/h-sl-ft
|
none
|
||||||
none
|
0 10000 20000 30000 40000 50000
|
||||||
0 10000 20000 30000 40000 50000
|
0.0 1.0000 0.7400 0.5340 0.3720 0.2410 0.1490
|
||||||
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
|
||||||
0.2 0.9340 0.6970 0.5060 0.3550 0.2310 0.1430
|
0.4 0.6210 0.5920 0.4060 0.3570 0.2330 0.1450
|
||||||
0.4 0.9210 0.6920 0.5060 0.3570 0.2330 0.1450
|
0.6 0.3510 0.2710 0.2020 0.1780 0.1020 0.0640
|
||||||
0.6 0.9510 0.7210 0.5320 0.3780 0.2480 0.1540
|
0.8 0.0200 0.0200 0.0200 0.0200 0.0200 0.0200
|
||||||
0.8 1.0200 0.7820 0.5820 0.4170 0.2750 0.1700
|
1.0 0.0 0.0 0.0 0.0 0.0 0.0
|
||||||
1.0 1.1200 0.8710 0.6510 0.4750 0.3150 0.1950
|
</TABLE>
|
||||||
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>
|
</FG_SIMTURBINE>
|
||||||
|
|
|
||||||
|
|
@ -10,9 +10,10 @@
|
||||||
augmented? no
|
augmented? no
|
||||||
injected? no
|
injected? no
|
||||||
-->
|
-->
|
||||||
|
<!-- 2500 horsepower X 2.24 lbs/hp -->
|
||||||
<FG_SIMTURBINE NAME="PW125B">
|
<FG_SIMTURBINE NAME="PW125B">
|
||||||
MAXMILTHRUST 4175.00
|
MILTHRUST 5600.00
|
||||||
|
MAXTHRUST 5600.00
|
||||||
BYPASSRATIO 0.0
|
BYPASSRATIO 0.0
|
||||||
TSFC 0.55
|
TSFC 0.55
|
||||||
ATSFC 0.0
|
ATSFC 0.0
|
||||||
|
|
@ -53,38 +54,4 @@
|
||||||
0.8 0.0200 0.0200 0.0200 0.0200 0.0200 0.0200
|
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
|
1.0 0.0 0.0 0.0 0.0 0.0 0.0
|
||||||
</TABLE>
|
</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>
|
</FG_SIMTURBINE>
|
||||||
|
|
|
||||||
|
|
@ -5,7 +5,8 @@
|
||||||
|
|
||||||
<FG_SIMTURBINE NAME="T76">
|
<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
|
BYPASSRATIO bypass ratio
|
||||||
TSFC thrust-specific fuel consumption (lbm/hr/lbf)
|
TSFC thrust-specific fuel consumption (lbm/hr/lbf)
|
||||||
ATSFC augmented TSFC (lbm/hr/lbf)
|
ATSFC augmented TSFC (lbm/hr/lbf)
|
||||||
|
|
@ -24,7 +25,8 @@
|
||||||
TABLE(3) water-injection multiplier vs. altitude and mach
|
TABLE(3) water-injection multiplier vs. altitude and mach
|
||||||
-->
|
-->
|
||||||
|
|
||||||
MAXMILTHRUST 1200
|
MILTHRUST 1600
|
||||||
|
MAXTHRUST 1600
|
||||||
BYPASSRATIO 0
|
BYPASSRATIO 0
|
||||||
TSFC 0.55
|
TSFC 0.55
|
||||||
ATSFC 0.00
|
ATSFC 0.00
|
||||||
|
|
@ -52,59 +54,19 @@
|
||||||
1.0 -0.2839 -0.1104 -0.0469 -0.0270 -0.0158 0.0552
|
1.0 -0.2839 -0.1104 -0.0469 -0.0270 -0.0158 0.0552
|
||||||
</TABLE>
|
</TABLE>
|
||||||
|
|
||||||
<!-- data from EngineSim, http://www.grc.nasa.gov/WWW/K-12/airplane/ngnsim.html -->
|
<TABLE NAME="MilThrust" TYPE="TABLE">
|
||||||
<TABLE NAME="MilThrust" TYPE="TABLE">
|
Military_power_thrust_factor
|
||||||
Military_power_thrust_factor
|
6
|
||||||
8
|
6
|
||||||
6
|
velocities/mach-norm
|
||||||
velocities/mach-norm
|
position/h-sl-ft
|
||||||
position/h-sl-ft
|
none
|
||||||
none
|
0 10000 20000 30000 40000 50000
|
||||||
0 10000 20000 30000 40000 50000
|
0.0 1.0000 0.7400 0.5340 0.3720 0.2410 0.1490
|
||||||
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
|
||||||
0.2 0.9340 0.6970 0.5060 0.3550 0.2310 0.1430
|
0.4 0.6210 0.5920 0.4060 0.3570 0.2330 0.1450
|
||||||
0.4 0.9210 0.6920 0.5060 0.3570 0.2330 0.1450
|
0.6 0.3510 0.2710 0.2020 0.1780 0.1020 0.0640
|
||||||
0.6 0.9510 0.7210 0.5320 0.3780 0.2480 0.1540
|
0.8 0.0200 0.0200 0.0200 0.0200 0.0200 0.0200
|
||||||
0.8 1.0200 0.7820 0.5820 0.4170 0.2750 0.1700
|
1.0 0.0 0.0 0.0 0.0 0.0 0.0
|
||||||
1.0 1.1200 0.8710 0.6510 0.4750 0.3150 0.1950
|
</TABLE>
|
||||||
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>
|
</FG_SIMTURBINE>
|
||||||
|
|
|
||||||
|
|
@ -12,7 +12,8 @@
|
||||||
-->
|
-->
|
||||||
|
|
||||||
<FG_SIMTURBINE NAME="Tay-650">
|
<FG_SIMTURBINE NAME="Tay-650">
|
||||||
MAXMILTHRUST 15400
|
MILTHRUST 15400
|
||||||
|
MAXTHRUST 15400
|
||||||
BYPASSRATIO 1.0
|
BYPASSRATIO 1.0
|
||||||
TSFC 0.8
|
TSFC 0.8
|
||||||
ATSFC 1.7
|
ATSFC 1.7
|
||||||
|
|
@ -55,38 +56,4 @@
|
||||||
1.2 1.2300 0.9750 0.7440 0.5450 0.3640 0.2250
|
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
|
1.4 1.3400 1.0860 0.8450 0.6280 0.4240 0.2630
|
||||||
</TABLE>
|
</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>
|
</FG_SIMTURBINE>
|
||||||
|
|
|
||||||
|
|
@ -1,18 +1,18 @@
|
||||||
<xml version="1.0"?>
|
<xml version="1.0"?>
|
||||||
<!-- Generated by Aero-Matic v 0.3
|
<!-- Generated by Aero-Matic v 0.7
|
||||||
|
|
||||||
Inputs:
|
Inputs:
|
||||||
horsepower: 2500
|
horsepower: 2250
|
||||||
pitch: variable
|
pitch: variable
|
||||||
|
|
||||||
Outputs:
|
Outputs:
|
||||||
linear-blade-inches: 265
|
linear-blade-inches: 251.40107398339
|
||||||
-->
|
-->
|
||||||
|
|
||||||
<FG_PROPELLER NAME="prop">
|
<FG_PROPELLER NAME="prop">
|
||||||
IXX 3.7910590942383
|
IXX 3.7910590942383
|
||||||
DIAMETER 144
|
DIAMETER 75
|
||||||
NUMBLADES 6
|
NUMBLADES 4
|
||||||
MINPITCH 10
|
MINPITCH 10
|
||||||
MAXPITCH 30
|
MAXPITCH 30
|
||||||
MINRPM 700
|
MINRPM 700
|
||||||
|
|
|
||||||
Loading…
Add table
Reference in a new issue