Jump to content
Sign in to follow this  
Guest pfunkmusik

Engine Question

Recommended Posts

Guest pfunkmusik

If I wanted to uprate the F-14A to F-14D status and give them the F110 turbofan (the same one that's in the Eagle), how do I do that?

 

pfunk

Share this post


Link to post
Share on other sites

you take a look in the Data.ini of your F-14 and change in section "engines" the existing entry with these:

 

[Engine1]

ReferenceName=General Electric F110_PW-400 Afterburning Turbofan

SystemType=JET_ENGINE

InputName=THROTTLE_CONTROL

EngineID=1

HasAfterburner=TRUE

NumAfterburnerStages=5

SLThrustDry=73895

SLThrustWet=120473

ThrustAngles=0.00,0.00,0.00

ThrustPosition=-1.4,0.00,0.00

ThrottleRate=0.5

NozzleAnimationID=2

ThrottleRate=0.5

NozzleAnimationID=6

IdleThrottle=0.10

IdleRPM=0.68

IdleNozzle=0.0

CruiseThrottle=0.37

CruiseRPM=0.82

CruiseNozzle=0.0

MilThrottle=0.65

MilRPM=1.00

MilNozzle=0.0

MaxThrottle=0.78

MaxRPM=1.00

MaxNozzle=0.0

FullABThrottle=1.12

FullABRPM=1.00

FullABNozzle=1.0

AltitudeTableNumData=10

AltitudeTableDeltaX=3048.0

AltitudeTableStartX=0.0

AltitudeTableData=1.000,0.802,0.634,0.496,0.381,0.288,0.206,0.147,0.105,0.000

DryMachTableNumData=4

DryMachTableDeltaX=0.4

DryMachTableStartX=0.0

DryMachTableData=1.000,0.980,1.172,0.000

WetMachTableNumData=7

WetMachTableDeltaX=0.4

WetMachTableStartX=0.0

WetMachTableData=1.000,0.991,1.207,1.683,2.473,2.750,3.02

MaxInletTemperature=120

GyroscopicInertia=

TSFCM0=0.820

TSFCM1=1.220

AfterburnerTSFC=1.940

MinFuelFlow=0.01

ExhaustEmitterName=F14ExhaustEmitter

ExhaustEffectSize=0.8

ExhaustPosition=-1.501,-8.0,-0.277

AfterburnerNodeName=BurnerOn

AfterburnerEmitterName=F16XLAfterburner

AfterburnerEffectSize=0.8

MinExtentPosition=-1.875,-4.166,-0.652

MaxExtentPosition=-0.96,-6.982, 0.156

FireSuppression=TRUE

GasTempMaxRPM=635.0

GasTempIdleRPM=420.0

GasTempChangeRate=5.0

OverheatTemp=750.0

DamageTempDelta=300.0

OilPressMaxRPM=35.0

OilPressIdleRPM=55.0

OilPressChangeRate=0.5

LowOilPress=12.0

LowOilTempDelta=400.0

 

[Engine2]

ReferenceName=General Electric F110_PW-400 Afterburning Turbofan

SystemType=JET_ENGINE

InputName=THROTTLE_CONTROL

EngineID=2

HasAfterburner=TRUE

NumAfterburnerStages=5

SLThrustDry=73895

SLThrustWet=120473

ThrustAngles=0.00,0.00,0.00

ThrustPosition=1.4,0.00,0.00

ThrottleRate=0.5

NozzleAnimationID=3

IdleThrottle=0.10

IdleRPM=0.68

IdleNozzle=0.0

CruiseThrottle=0.37

CruiseRPM=0.82

CruiseNozzle=0.0

MilThrottle=0.65

MilRPM=1.00

MilNozzle=0.0

MaxThrottle=0.78

MaxRPM=1.00

MaxNozzle=0.0

FullABThrottle=1.12

FullABRPM=1.00

FullABNozzle=1.0

AltitudeTableNumData=10

AltitudeTableDeltaX=3048.0

AltitudeTableStartX=0.0

AltitudeTableData=1.000,0.802,0.634,0.496,0.381,0.288,0.206,0.147,0.105,0.000

DryMachTableNumData=4

DryMachTableDeltaX=0.4

DryMachTableStartX=0.0

DryMachTableData=1.000,0.980,1.172,0.000

WetMachTableNumData=7

WetMachTableDeltaX=0.4

WetMachTableStartX=0.0

WetMachTableData=1.000,0.991,1.207,1.683,2.473,2.750,3.02

MaxInletTemperature=120

GyroscopicInertia=

TSFCM0=0.820

TSFCM1=1.220

AfterburnerTSFC=1.940

MinFuelFlow=0.01

ExhaustEmitterName=F14ExhaustEmitter

ExhaustEffectSize=0.8

ExhaustPosition=1.501,-8.0,-0.277

AfterburnerNodeName=BurnerOn

AfterburnerEmitterName=F16XLAfterburner

AfterburnerEffectSize=0.8

MinExtentPosition=1.875,-4.166,-0.652

MaxExtentPosition=0.96,-6.982, 0.156

FireSuppression=TRUE

GasTempMaxRPM=635.0

GasTempIdleRPM=420.0

GasTempChangeRate=5.0

OverheatTemp=750.0

DamageTempDelta=300.0

OilPressMaxRPM=35.0

OilPressIdleRPM=55.0

OilPressChangeRate=0.5

LowOilPress=12.0

LowOilTempDelta=400.0

 

or you just go to the Download Section and download the F-14D V1.4 by Typhoid. :biggrin:

Share this post


Link to post
Share on other sites

Create an account or sign in to comment

You need to be a member in order to leave a comment

Create an account

Sign up for a new account in our community. It's easy!

Register a new account

Sign in

Already have an account? Sign in here.

Sign In Now
Sign in to follow this  

×

Important Information

By using this site, you agree to our Terms of Use, Privacy Policy, and We have placed cookies on your device to help make this website better. You can adjust your cookie settings, otherwise we'll assume you're okay to continue..