46 lines
1.6 KiB
XML
46 lines
1.6 KiB
XML
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<?xml version="1.0"?>
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<!-- CFM56 turbofan engine model
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Version 0.9, 31 Jan 2003, David Culp, davidculp2@attbi.com
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_______________________________________________________________
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-->
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<FG_TURBINE NAME="CFM56">
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<!-- max static thrust at S.L. (installed), lbs -->
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MAXMILTHRUST 19000
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<!-- augmentation not installed -->
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MAXAUGTHRUST 19000
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<!-- Idle Thrust -->
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<TABLE NAME="IdleThrust" TYPE="TABLE">
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Idle_power_thrust_factor
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6
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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 0.0836 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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0.4 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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0.8 -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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</TABLE>
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<TABLE NAME="MilThrust" TYPE="TABLE">
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Effects_of_altitude_and_mach_on_thrust
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7
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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 1.0000 0.7216 0.4890 0.3115 0.1932 0.1104
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0.2 1.0000 0.7216 0.4979 0.3186 0.1948 0.1104
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0.4 0.9945 0.7344 0.5213 0.3383 0.2050 0.1230
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0.6 0.9968 0.7759 0.5591 0.3675 0.2240 0.1309
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0.8 0.9771 0.8025 0.6112 0.4196 0.2563 0.1522
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0.9 0.9300 0.7900 0.6000 0.3900 0.2300 0.1300
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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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</FG_TURBINE>
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