Afterburner thrust

Posted:
Sun Nov 29, 2009 8:16 pm
by brettt777
Where is the thrust of the afterburner determined? I have some planes, like the Accel pack F-18, that the afterburner seems very realistic. When it kicks in, there is an obviously large increase in the thrust. But I have other planes where the AB makes very little difference if any. The only increase in thrust is the small amount the throttle is moved to go from 95% or 98% to 100%.
Re: Afterburner thrust

Posted:
Sun Nov 29, 2009 8:23 pm
by Tai-2
Here is what one of the ABs look on one of my planes in the cfg file
[TurbineEngineData]
fuel_flow_gain=0.012
inlet_area=5.0
rated_N2_rpm=18000.0
static_thrust=11875.0
afterburner_available=1
reverser_available=0
here is the Accelerations
[TurbineEngineData]
fuel_flow_gain = 0.006 //Gain on fuel flow
inlet_area = 4.2895 //Square Feet, engine nacelle inlet area
rated_N2_rpm = 16728 //RPM, second stage compressor rated value
static_thrust = 11000 //Lbs, max rated static thrust at Sea Level
afterburner_available = 6 //Afterburner stages available?
afterburner_throttle_threshold = 0.80 //Percent of throttle range where a/b begins
reverser_available = 0 //Thrust reverser available?
ThrustSpecificFuelConsumption = 0.81 //Thrust specific fuel consumption (Jets)
AfterBurnThrustSpecificFuelConsumption = 1.74 //TSFC with afterburn/reheat engaged
from the look of it you want the static_thrust ithink. not sure but it is worth a try