J
Hello Friends;
I want to discuss here the corrected parameters of Gas Turbine two shaft. I read many articles in which it describe that
NGP corrected = NGP/ Sqrt(T1/Tstd), T in Deg R
I examine that Power turbine speed is not corrected with this formula because i check when T7 (Exhaust Temperature) drop or increase it effects the corrected speed of power turbine in two shaft turbine.
Also how to correct Power, Mass flow and fuel flow?
If any friend have document in which example is given please send me.
Best regards
I want to discuss here the corrected parameters of Gas Turbine two shaft. I read many articles in which it describe that
NGP corrected = NGP/ Sqrt(T1/Tstd), T in Deg R
I examine that Power turbine speed is not corrected with this formula because i check when T7 (Exhaust Temperature) drop or increase it effects the corrected speed of power turbine in two shaft turbine.
Also how to correct Power, Mass flow and fuel flow?
If any friend have document in which example is given please send me.
Best regards
