<?xml version="1.0"?> <!-- CFM56 turbofan engine model Version 0.9, 31 Jan 2003, David Culp, davidculp2@attbi.com _______________________________________________________________ --> <FG_TURBINE NAME="CFM56"> <!-- max static thrust at S.L. (installed), lbs --> MAXMILTHRUST 19000 <!-- augmentation not installed --> MAXAUGTHRUST 19000 <!-- Idle Thrust --> <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> </FG_TURBINE>