Aerospace Engineering > GATE 2021 > Shock Waves
A shock moving into a stationary gas can be transformed to a stationary shock by a change in reference frame, as shown in the figure. Which of the following is/are true relating the flow properties in the two reference frames?
A
T'1 > T1, T'01 > T01, p'01 > p01, ρ'2 > ρ'1
B
T'1 = T1, T'2 < T01, p'01 > p01, ρ'2 = ρ2
C
T'1 < T1, p'1 > p1, p'01 > p01, ρ'2 > ρ1
D
T'1 = T1, p2 > p01, T'01 > T01, p'01 > p01

Correct : d

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Related Topics

shock wave reference frame GATE Aerospace Engineering 2021 shock moving into stationary gas stationary shock transformation flow properties reference frames aerospace engineering gate shock wave properties GATE 2021 set 33

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