Question: When a sea-level air flow approaches a ramp of angle 20°, an oblique shock wave forms as in Figure P9.124 Calculate (a) Ma1; (b) P2;
(a) Ma1;
(b) P2;
(c) T2; and (d) V2.
40 20
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For sealevel air take p1 10135 kPa T1 28816 K and 1 12255 kgm3 a The a... View full answer
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