Compressible Flow
Air enters a nozzle operating at steady state at 45 lbf/in.2, 800°R, with a velocity of 480 ft/s, and expands isentropically to an exit velocity of 1500 ft/s. Using data from Table A-22E as needed, determine
(a) the exit pressure, in lbf/in.2
(b) the ratio of the exit area to the inlet area.
(c) whether the nozzle is diverging only, converging only, or converging–diverging in cross section.
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