<?xml version="1.0"?> <!-- File: Tay-650.xml Author: Aero-Matic v 0.2 Inputs: name: Tay-650 type: turbine thrust: 15400 lb augmented? no injected? no --> <FG_SIMTURBINE NAME="Tay-650"> MAXMILTHRUST 15400 BYPASSRATIO 1.0 TSFC 0.8 ATSFC 1.7 IDLEN1 30.0 IDLEN2 60.0 MAXN1 100.0 MAXN2 100.0 AUGMENTED 0 AUGMETHOD 1 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 0.1342 0.4 0.0047 0.0020 0.0272 0.0595 0.0891 0.1203 0.6 0.0 0.0 0.0 0.0276 0.0718 0.1073 0.8 0.0 0.0 0.0 0.0 0.0474 0.0868 1.0 0.0 0.0 0.0 0.0 0.0 0.0552 </TABLE> <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> </FG_SIMTURBINE>