If you change the engine type, you also need to change all of the engine parameters to be appropriate to that type.Garry Russell wrote:So.......will changing the type affect the performance or is there something else on the go here??
Tucano AI will not take off!!
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Re: Tucano AI will not take off!!
George


- Garry Russell
- The Ministry
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Re: Tucano AI will not take off!!
OK
That then goes back to my original thought
Thanks
That then goes back to my original thought
Thanks

Garry

"In the world of virtual reality things are not always what they seem."

"In the world of virtual reality things are not always what they seem."
Re: Tucano AI will not take off!!
This is the standard engine data
[GeneralEngineData]
engine_type = 1
Engine.0 = -18.0, 0, 1.468
fuel_flow_scalar = 1
min_throttle_limit=0.000000
[TurbineEngineData]
fuel_flow_gain = 0.0021
inlet_area = 0.6333
rated_N2_rpm = 13500 //rpm @ 100%
static_thrust = 2250 //(Dry)
afterburner_available = 0
reverser_available = 1
[jet_engine]
thrust_scalar = 1.0
and this is my modified one
[GeneralEngineData]
engine_type =5
fuel_flow_scalar = 1
min_throttle_limit=0.00000
engine.0 = -18.0, 0, 1.468
[TurbineEngineData]
static_thrust = 2250 //(Dry)
inlet_area = 0.6333
rated_N2_rpm = 13500 //rpm @ 100%
fuel_flow_gain = 0.0021
reverser_available = 1
afterburner_available = 0
[turboprop_engine]
maximum_torque=1000.00000
power_scalar=1.0
It now taxies and takes off and flys ok...but when coming into land at 700ft onwards on approach the aircraft goes up and down in altitude then crashes into the runway and vanishes,any ideas??
[GeneralEngineData]
engine_type = 1
Engine.0 = -18.0, 0, 1.468
fuel_flow_scalar = 1
min_throttle_limit=0.000000
[TurbineEngineData]
fuel_flow_gain = 0.0021
inlet_area = 0.6333
rated_N2_rpm = 13500 //rpm @ 100%
static_thrust = 2250 //(Dry)
afterburner_available = 0
reverser_available = 1
[jet_engine]
thrust_scalar = 1.0
and this is my modified one
[GeneralEngineData]
engine_type =5
fuel_flow_scalar = 1
min_throttle_limit=0.00000
engine.0 = -18.0, 0, 1.468
[TurbineEngineData]
static_thrust = 2250 //(Dry)
inlet_area = 0.6333
rated_N2_rpm = 13500 //rpm @ 100%
fuel_flow_gain = 0.0021
reverser_available = 1
afterburner_available = 0
[turboprop_engine]
maximum_torque=1000.00000
power_scalar=1.0
It now taxies and takes off and flys ok...but when coming into land at 700ft onwards on approach the aircraft goes up and down in altitude then crashes into the runway and vanishes,any ideas??