On Friday 17 June 2011 08:15:36 xsaint wrote: > Thank you Emilian and Buck.... > > Ok i tested changing the location of the point to ahead of the engine > and also behind the engine, near exhaust. > Irrespective of the location, looking at the results at the Yasim > solver, i do not see much impact. > > Surprisingly i do not see any change to Drag Coef or lift ratio. > The only slight change seems to occur rightfully at Tail incidence and > approach elevator... > > Is this how it is ment to be? > > Cheers > You'll most likely see the differences in flight, in asymetric configurations. AFAIK the solver uses just the thrust value, and of course the engine weight for COG determination.
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