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Flow at Mach 3 reaches a 20º deflection, which creates an oblique shock with supersonic flow on both sides. Downstream of the

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M,= 3 , = 20° 19 B, = 37.7636° ( By A-B-M, se diagram ! Min = M, Senß, = 1.8.372 M2n = 0.60839 (Normal shock, T2 - 1.559 69 rTis 288.16.K , standard sea level condition) Tzz 4.49.414k Tz = 7.56.838) K M2=2 Mizzil 1 hearest integen 3 IN NI 288 K 49 kplease rate me high.....................

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