diff --git a/Engine/Tay-651_sim.xml b/Engine/Tay-651_sim.xml
new file mode 100644
index 000000000..e7ef04351
--- /dev/null
+++ b/Engine/Tay-651_sim.xml
@@ -0,0 +1,92 @@
+<?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>