A normal shock wave propagates into atmosphere where the atmospheric temperature is equal to T₁ = 336K and pressure is 0.8 atm. For a given pressure ratio of p2/p₁ = 41 a) Assuming stationary atmosphere, calculate the shock wave velocity and the velocity induced behind the shock wave. Also calculate the temperature, total pressure and total temperature of the fluid particles behind the shock wave using equations for moving normal shock.

A normal shock wave propagates into atmosphere where the atmospheric temperature is equal to T₁ = 336K and pressure is 0.8 atm. For a given pressure ratio of p2/p₁ = 41 a) Assuming stationary atmosphere, calculate the shock wave velocity and the velocity induced behind the shock wave. Also calculate the temperature, total pressure and total temperature of the fluid particles behind the shock wave using equations for moving normal shock.

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

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A normal shock wave propagates into atmosphere where the atmospheric temperature is equal
336K
and pressure is 0.8 atm. For a given pressure ratio of p2/p₁ 41
to T₁ =
a)
Assuming stationary atmosphere, calculate the shock wave velocity and the velocity induced behind
the shock wave. Also calculate the temperature, total pressure and total temperature of the fluid
particles behind the shock wave using equations for moving normal shock.
=

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