Aerospace Engineering > GATE 2013 > Isentropic Flow
Consider one-dimensional isentropic flow at a Mach number of 0.5. If the area of cross-section of a streamtube increases by 3% somewhere along the flow, the corresponding percentage change in density is

Correct : -2.0 to -1.9

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one-dimensional isentropic flow isentropic flow density change Mach number 0.5 streamtube area increase Aerospace Engineering GATE 2013 GATE AE 2013 Q33 compressible flow fluid mechanics

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