The Mach number at inlet of gas turbine diffuser is 0.3. The shape of the diffuser would be:

The Mach number at inlet of gas turbine diffuser is 0.3. The shape of

1.	The Mach number at inlet of gas turbine diffuser is 0.3. The shape of the diffuser would be:
A.	Converging
B.	diverging I
C.	Stagnation enthalpy
D.	stagnation pressure
Answer» C. Stagnation enthalpy

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The Mach number at inlet of gas turbine diffuser is 0.3. The shape of the diffuser would be:

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