diff --git a/Aircraft/737-jsbsim-set.xml b/Aircraft/737-jsbsim-set.xml
index 1ca412c92..81a04a239 100644
--- a/Aircraft/737-jsbsim-set.xml
+++ b/Aircraft/737-jsbsim-set.xml
@@ -3,10 +3,8 @@
Boeing 737
-
jsb
737
- 0.5
@@ -20,17 +18,17 @@
- Aircraft/737/Panels/737-trans-mini-panel.xml
+ Aircraft/T38/Panels/T38-panel.xml
true
- Huds/737/default.xml
- true
+ Huds/Default/default.xml
+ false
- Aircraft/747/Models/boeing747-400-jw.xml
+ Aircraft/T38/Models/T38-model.xml
@@ -39,9 +37,23 @@
+
+
+
+ 1490
+
+
+ 1490
+
+
+ 2230
+
+
+
+
- 150.0
+ 210.0
300.0
2000.0
1500.0
@@ -50,7 +62,7 @@
0.0001
0.0001
30
- 1.0
+ 0.4
diff --git a/Aircraft/OV10-jsbsim-set.xml b/Aircraft/OV10-jsbsim-set.xml
index 65eb0df2c..0311c1965 100644
--- a/Aircraft/OV10-jsbsim-set.xml
+++ b/Aircraft/OV10-jsbsim-set.xml
@@ -37,7 +37,7 @@ David Culp, davidculp2@attbi.com
-
+
117
@@ -49,6 +49,6 @@ David Culp, davidculp2@attbi.com
220
-
+
diff --git a/Aircraft/T38-jsbsim-set.xml b/Aircraft/T38-jsbsim-set.xml
new file mode 100644
index 000000000..705ae3d65
--- /dev/null
+++ b/Aircraft/T38-jsbsim-set.xml
@@ -0,0 +1,52 @@
+
+
+
+
+
+
+
+ Northrop T-38
+
+ jsb
+ T38
+
+
+
+ Aircraft/c172/c172-electrical.xml
+
+
+
+
+ true
+ Aircraft/T38/Sounds/T38-sound.xml
+
+
+
+ Aircraft/T38/Panels/T38-panel.xml
+ true
+
+
+
+
+ Aircraft/T38/Models/T38-model.xml
+
+
+
+
+
+
+
+ 280
+
+
+ 280
+
+
+
+
+
diff --git a/Aircraft/T38-set.xml b/Aircraft/T38-set.xml
index 0396c1b32..a377201de 100644
--- a/Aircraft/T38-set.xml
+++ b/Aircraft/T38-set.xml
@@ -1,42 +1,7 @@
-
-
-
+
-
- Northrop T-38
-
- jsb
- T38
-
-
-
- Aircraft/c172/c172-electrical.xml
-
-
-
-
- true
- Aircraft/T38/Sounds/T38-sound.xml
-
-
-
- Aircraft/T38/Panels/T38-panel.xml
- true
-
-
-
-
- Aircraft/T38/Models/T38-model.xml
-
-
-
+ Alias for T38-jsbsim.
-
diff --git a/Aircraft/t6texan2-jsbsim-set.xml b/Aircraft/t6texan2-jsbsim-set.xml
index b3b39e216..3805e31f3 100644
--- a/Aircraft/t6texan2-jsbsim-set.xml
+++ b/Aircraft/t6texan2-jsbsim-set.xml
@@ -11,16 +11,16 @@ David Culp, davidculp2@attbi.com
T-6A Texan II
-
+
jsb
t6texan2
-
+
Aircraft/c172/c172-electrical.xml
-
+
true
Aircraft/t6texan2/Sounds/t6texan2-sound.xml
@@ -35,7 +35,17 @@ David Culp, davidculp2@attbi.com
Aircraft/t6texan2/Models/T6Texan2.mdl
-
+
+
+
+ 73
+
+
+ 73
+
+
+
+
diff --git a/Engine/F100-PW-229_sim.xml b/Engine/F100-PW-229_sim.xml
new file mode 100644
index 000000000..dd068097e
--- /dev/null
+++ b/Engine/F100-PW-229_sim.xml
@@ -0,0 +1,111 @@
+
+
+
+
+
+
+
+ MAXMILTHRUST 17800
+ BYPASSRATIO 0.4
+ TSFC 0.74
+ ATSFC 2.05
+ IDLEN1 40.0
+ IDLEN2 53.0
+ MAXN1 100.0
+ MAXN2 100.0
+ AUGMENTED 1
+ AUGMETHOD 1
+ INJECTED 0
+
+
+ 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
+
+
+
+
+ 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
+
+
+
+
+ Augmented_thrust_factor
+ 8
+ 6
+ velocities/mach-norm
+ position/h-sl-ft
+ none
+ 0 10000 20000 30000 40000 50000
+ 0.0 1.6290 1.6290 1.6290 1.6290 1.6290 1.6290
+ 0.2 1.6290 1.6290 1.6290 1.6290 1.6290 1.6290
+ 0.4 1.6290 1.6290 1.6290 1.6290 1.6290 1.6290
+ 0.6 1.6290 1.6290 1.6290 1.6290 1.6290 1.6290
+ 0.8 1.6290 1.6290 1.6290 1.6290 1.6290 1.6290
+ 1.0 1.6290 1.6290 1.6290 1.6290 1.6290 1.6290
+ 1.2 1.6290 1.6290 1.6290 1.6290 1.6290 1.6290
+ 1.4 1.6290 1.6290 1.6290 1.6290 1.6290 1.6290
+
+
+
+ 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
+
+
+