Downstream of the shock the flow is isentropic the mach


Air as an ideal gas with k = 1.4 enters a converging- diverging channel at a Mach number of 1.2. A normal shock stands at the inlet to the channel. Downstream of the shock the flow is isentropic; the Mach number is unity at the throat; and the air exits at 100 lbf/in.2 , 540 °R, with negligible velocity. If the mass flow rate is 100 lb/s, determine the inlet and throat areas, in ft2 .

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Econometrics: Downstream of the shock the flow is isentropic the mach
Reference No:- TGS01644738

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