Aerospace Engineering > GATE 2014 > Normal Shock Waves
A student needs to find velocity across a stationary normal shock. He measures density and pressure across the shock as shown in the figure below. 1bar=105Pa. (No shock table is needed for the calculations). The value of u1 in m/s is

Correct : 1705 to 1720

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normal shock velocity stationary normal shock velocity across shock aerospace engineering gate 2014 shock wave velocity pressure density shock GATE Aerospace Engineering 2014 shock velocity calculation

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