How does the diffuser produce thrust in in a jet engine? : r/AerospaceEngineering
As shown, air enters the diffuser of a jet engine at 18 kPa, 216 K with a velocity of 265 m/s, all data corresponding to high altitude flight. The air flows adiabatically
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4.37 As shown in Fig. P4.37, air enters the diffuser of a jet engine operating at steady state at 18 - YouTube