(AERO50009 Propulsion, Department of Aeronautics, Imperial College London).

Turbojet h-s diagram comparison

M = Ta= T0b= prc = ηd= ηc = ηt= ηn = rb =

M = Ta= T0b= prc = ηd= ηc = ηt= ηn = rb =

In fact, here T is plotted vs exp(s/cp). Keep the parameters within a reasonable range.

Originally developed by A.Chernyshenko, modified by S.Chernyshenko