Find the velocity downstream of the shock

Reference no: EM131352473

Air at 290°K and 105 P a approaches a normal shock. The temperature downstream of the shock is 540°K. Find:

(a) The velocity downstream of the shock.

(b) The pressure change across the shock, and compare it with that calculated for an isentropic flow with the same deceleration.

Reference no: EM131352473

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