Engineering, 14.12.2021 03:00, kyla1220

Find the Mach number and air speed corresponding of 500 kPa(abs) in an air flow with a (static) pressure of 100 kPa and measured (stagnation) temperature of 500 K. DISCUSSION: Suppose that, instead of assuming that a normal shock occurs upstream of the Pitot tube, it is assumed that the flow upstream is ISENTROPIC... what would the estimated flow speed be in that case? (NOTE: A normal shock is always observed to form upstream of bluff bodies such as Pitot tubes in supersonic flow.) to a Pitot tube stagnation pressure measurement

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Find the Mach number and air speed corresponding of 500 kPa(abs) in an air flow with a (static) pres...