In the F-35
[TurbineEngineData]
fuel_flow_gain = 0.046 //Gain on fuel flow
inlet_area = 6.000 //Square Feet, engine nacelle inlet area - Approximate from 3d model
rated_N2_rpm = 16728 //RPM, second stage compressor rated value
static_thrust = 28000 //Lbs, max rated static thrust at Sea Level - Should be 28,000 but was lowered due to excessive acceleration - Note, this combined with air file values produces a maximum thust (with A/B) of about 37500lbs (actual value should be 42,000+)
afterburner_available =
3 //Afterburner stages available?
afterburner_throttle_threshold = 0.90 //Percent of throttle range where a/b begins
reverser_available = 0 //Thrust reverser available?
ThrustSpecificFuelConsumption = 0.80 //Thrust specific fuel consumption (Jets) Exact value should be 0.886 correct from wiki, adjusted after long range tests
AfterBurnThrustSpecificFuelConsumption = 1.82 //TSFC with afterburn/reheat engaged
It beats me where they are getting the effects from or use. I think the effects are baked into the MDL's.
I sure do like what you've done with improvements of the F8 AB effect and appreciate your efforts