Question: 3 . 2 . 8 A shock wave is a very thin layer ( thickness = l ) in a highspeed ( supersonic ) gas
A shock wave is a very thin layer thickness in a highspeed supersonic gas flow across which the flow properties velocity density, pressure, etc. change from state to state as shown in Fig. P If and estimate the average deceleration of the gas as it flows across the shock wave. How many gs deceleration does this represent?
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