<?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>