When a sea level air flow approaches a ramp of angle 20 deg , an oblique shock wave forms as in Figure P9 124 Calculate (a) Ma1 (b) P2 (c) T2 and (d) V2 40 20...

For sealevel air take p1 10135 kPa T1 28816 K and 1 12255 kgm3 a The a ...

When a sea-level air flow approaches a ramp of angle 20°, an oblique shock wave forms as

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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;
(c) T2; and (d) V2.

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Fundamentals of Aerodynamics

ISBN: 978-0070016798

2nd Edition

Authors: J. Anderson

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Question Posted: Jan 20, 2010 02:50 AM

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When a sea-level air flow approaches a ramp of angle 20°, an oblique shock wave forms as

Question:

40° 20°

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Fundamentals of Aerodynamics

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