- Aerodynamics

p_B = 2p_e

p_B = p_e

p_B < p_e

p_B > p_e

Correct Answer :

Recently Updated in Aerodynamics Questions

What is the relation between the nozzle A_1t and diffuser throat area A_2t in the supersonic wind tunnel?

A_t2 = A_t1

A_t2 < A_t1

A_t2 > A_t1

A_t2 A_t1 = 1

Correct Answer : Option (C) : A_t2 > A_t1

In which scenario is the throat area of both the nozzle and diffuser the same?

Ideal isobaric diffuser

Ideal isentropic diffuser

Ideal Isochoric diffuser

Ideal adiabatic diffuser

Correct Answer : Option (B) : Ideal isentropic diffuser

What is the ratio of throat area of diffuser to nozzle in supersonic wind tunnel with flow at Mach 2.7?

0.4236

0.8338

1.199

2.36

Correct Answer : Option (D) : 2.36

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