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 +
+ +