On August 24, 2010 01:16:43 am Ron Jensen wrote:
> I am far from an expert on turbine engines, or the JSBSim turbine model,
>  but here it goes: (I'll use the f16 engine file, F100-PW-229.xml, as an
>  example)
> 
> Idle thrust is the factor from the IdleThrust table multiplied by the value
>  in the <milthrust> tag.  So, at Mach 0 at Sea Level, the running engine
>  produces
> 
>   0.0488 * 17800.0 lbs = 869 lbs idle thrust
> 
> and
> 
>  1.0000 * (17800.0 - 869 idle thrust) lbs =  16931 lbs mil thrust
> 
> N2norm is derived from the throttle position.   It is essentially just a
>  lag filtered throttle command.   We square the N2norm value, which is
>  between 0.0 and 1.0, multiply that by the mil thrust value, which is
>  reduced from the configured value by the amount of idle thrust (previous
>  equation), then add the idle thrust back in
> 
>  thrust = idlethrust + (milthrust * N2norm^2);
> 
> so the engine varies between
> 
>   869 lbs + ( 16931 lbs * 0.0^2) = 869 lbs thrust
> 
> and
> 
>  869 lbs + ( 16931 lbs * 1.0^2) = 17800 lbs thrust
> 
> If the afterburner is on (a.k.a, augmentation or reheat) the AugThrust
>  table is used in conjunction with the MaxThrust tag to increase the thrust
>  available using throttle position (we are in augmeathod = 2).  Augmethod
>  =1 simply replaces the above thrust calculation with the prodoct of the
>  AugThrust table value and the MaxThrust tag with no control available.
> 
> Hope that wasn't too unclear?
> 
> Questions?
> 
> Ron

I think this is what I need to work with.  Thank you very much.


Ampere

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