In Rayleigh flow at subsonic Mach numbers, heat addition

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asked Jan 17, 2018 in PPE by chandu (215k points)

In Rayleigh flow at subsonic Mach numbers, heat addition

(A) Decreases static pressure

(B) Decreases enthalpy

(C) Increases static pressure

(D) Decreases static temperature

ies-objectives-1
2011
ppe
jet-propulsion&compressible-flow

In Rayleigh flow at subsonic Mach numbers, heat addition

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