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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