Related InterviewSolutions

• Why can’t build an ideal supersonic diffuser with no total pressure losses?(a) Presence of shock waves(b) Varying cross – sectional area(c) Varying throat area(d) Choked flowThe question was asked in a job interview.I would like to ask this question from Quasi-One-Dimensional Flow Diffusers topic in section Quasi-One-Dimensional Flow of Aerodynamics
• What is the diffuser efficiency of a normal shock diffuser?(a) 1(b) 0(c) Inifinty(d) \(\frac {1}{2}\)The question was asked in my homework.I want to ask this question from Quasi-One-Dimensional Flow Diffusers in division Quasi-One-Dimensional Flow of Aerodynamics
• How is flow deaccelerated In the diffuser?(a) Isentropic compression(b) Isentropic expansion(c) Adiabatic compression(d) Adiabatic expansionI have been asked this question in examination.Question is from Quasi-One-Dimensional Flow Diffusers in chapter Quasi-One-Dimensional Flow of Aerodynamics
• In the area – Mach relation A < A^* or A ≥ A^*.(a) True(b) FalseThe question was posed to me in a national level competition.The doubt is from Nozzles in chapter Quasi-One-Dimensional Flow of Aerodynamics
• Which equation is obtained when Mach number is equated to zero in area-velocity relation?(a) Momentum equation(b) Continuity equation(c) Energy equation(d) Bernoulli’s equationI got this question in semester exam.My doubt stems from Area-Velocity Relation in chapter Quasi-One-Dimensional Flow of Aerodynamics
• Sonic flow exists at the throat of an equilibrium chemically reacting nozzle flow?(a) True(b) FalseThe question was asked in a national level competition.My question comes from Area-Velocity Relation in portion Quasi-One-Dimensional Flow of Aerodynamics
• Which is the Euler’s equation for the quasi – one dimensional flow?(a) dp = \(\frac {ρ}{u}\)du(b) dp = –\(\frac {u}{ρ}\)du(c) dp = -ρudu(d) dp = ρuduThe question was asked in semester exam.This interesting question is from Governing Equations in portion Quasi-One-Dimensional Flow of Aerodynamics
• In which of these conditions there’s no formation of shock wave inside a convergent – divergent nozzle?(a) Overexpanded(b) Underexpanded(c) Fully expanded(d) Fully underexpandedI have been asked this question by my college director while I was bunking the class.I'd like to ask this question from Nozzles topic in portion Quasi-One-Dimensional Flow of Aerodynamics
• Why is the diffuser throat area greater than the nozzle throat area?(a) To reduce speed(b) To maintain constant mass flow rate(c) Rise in entropy within diffuser(d) Rise in entropy within nozzleI had been asked this question in a job interview.Enquiry is from Quasi-One-Dimensional Flow Diffusers topic in chapter Quasi-One-Dimensional Flow of Aerodynamics
• Oblique shock diffuser has a better pressure recovery than a normal shock diffuser.(a) True(b) FalseThe question was posed to me in examination.My query is from Quasi-One-Dimensional Flow Diffusers in portion Quasi-One-Dimensional Flow of Aerodynamics