Question: Air flows supersonically over a circular-arc surface as in Fig. P9.148. Estimate (a) The Mach number Ma2 and (b) The pressure p2 as the flow
(a) The Mach number Ma2 and
(b) The pressure p2 as the flow leaves the circular surface.
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a At the initial condition Ma1 25 from Table B5 read 1 3912 a Circular ... View full answer
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