Compressible Flow
A converging–diverging nozzle operates at steady state. Air as an ideal gas with k = 1.4 flows through the nozzle, discharging to the atmosphere at 14.7 lbf/in.2 and 520°R. A normal shock stands at the exit plane with Mx = 1.5. The exit plane area is 1.8 in.2 Upstream of the shock, the flow is isentropic. Determine
(a) the stagnation pressure pox, in lbf/in.2
(b) the stagnation temperature Tox, in °R.
(c) the mass flow rate, in lb/s.
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