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Old 4th Nov 2014, 16:59
  #52 (permalink)  
Join Date: May 2014
Location: In thin air
Posts: 186

Nice try but no, I'm with Owain. If you are familiar with non-dimensional representation of turbojet engine performance, then it will be apparent that gross thrust and net thrust at a given altitude are defined by N1/root theta and Mach number. Mach number at a given altitude and IAS does not change with temperature.

Last edited by Gysbreght; 4th Nov 2014 at 17:09.
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