statira

thanks for your answer I totally understand now :)

Thanks so much! I mean , when blade angles is changed and what extend? Did change the angle of the exhaust gas? if yes when? So, I realized your words that engine components(such as, prop blade or nozzle geometry or etc.) never have changed. :confused: best regards statira

Hi Can someone tell me that, how change engine (T56-A-9) components with different flight conditions? Is the angle of compressor blades or nozzle geometry changed? Thanks