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Assume ideal gas, air gamma = 1.4, R = 287 J/kgK.

~ Use normal shock tables! ~

A pitot-static probe designed for subsonic flow shows the velocity calculated from the ratio of stagnation pressure to static

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Given. T= 350k M =% C=.To. Pstatic 8=114 ca speed of sound. - R = 0.287 kJ /kgk FORT V static = V1.4% 287 g 350 c = 375m/s PsPstagnation 2 8 Patah i ti ( 4 + =) 1.8214=/2x1um 2 .4 20 - 1.40²-02 M = 0.9659 Mz y y z 375X0.9659 Vindicated = 362 206 mis

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