<?xml version="1.0"?> <!-- CFM56-5 turbofan engine model Version 1.0, 4 Jun 2003, David Culp, davidculp2@attbi.com --> <FG_SIMTURBINE NAME="CFM56_5"> <!-- MAXMILTHRUST max static thrust at S.L. (installed), lbf BYPASSRATIO bypass ratio TSFC thrust-specific fuel consumption (lbm/hr/lbf) ATSFC augmented 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 INJECTED =1 if water injection installed, else =0 TABLE(0) idle thrust vs. altitude and mach TABLE(1) maximum un-augmented thrust vs. altitude and mach TABLE(2) augmented thrust multiplier vs. altitude and mach TABLE(3) water-injection multiplier vs. altitude and mach --> MAXMILTHRUST 25000 BYPASSRATIO 5.9 TSFC 0.657 ATSFC 0.0 IDLEN1 30.0 IDLEN2 60.0 MAXN1 100.0 MAXN2 100.0 AUGMENTED 0 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 0.1341 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 </TABLE> <TABLE NAME="MilThrust" TYPE="TABLE"> Effects_of_altitude_and_mach_on_thrust 7 6 velocities/mach-norm position/h-sl-ft none 0 10000 20000 30000 40000 50000 0.0 1.0000 0.7216 0.4890 0.3115 0.1932 0.1104 0.2 1.0000 0.7216 0.4979 0.3186 0.1948 0.1104 0.4 0.9945 0.7344 0.5213 0.3383 0.2050 0.1230 0.6 0.9968 0.7759 0.5591 0.3675 0.2240 0.1309 0.8 0.9771 0.8025 0.6112 0.4196 0.2563 0.1522 0.9 0.9300 0.7900 0.6000 0.3900 0.2300 0.1300 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>