Report - Introduction to Aerospace Engineering · 2016. 11. 7. · V= 1208 m/s M1=4 1 Bow shock wave P 2= 2347 N/m2 T 2 = 953 K P 3= 1240 N/m2 P 4= 704 N/m2 T= ? V= ? M= ? In 3,4 Boundary

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