Related InterviewSolutions

• Which condition is to be met for occurrence of stagnation point on a conical surface at an angle of attack with free stream? (Vθ, Vϕ are cross flow velocities)(a) Vθ + Vϕ = 1(b) Vθ + Vϕ = 0(c) Vθ^2 + Vϕ^2 = 0(d) (Vθ + Vϕ)^2 = 1I got this question in semester exam.I would like to ask this question from Cones at Angle of Attack in portion Three-Dimensional Flow of Aerodynamics
• When the angle of attack of the cone with free stream flow is greater than the shock wave angle where is the vortical singularity present?(a) On the windward surface(b) Away from the surface(c) Inside the conical surface(d) On the leeward surfaceI have been asked this question in unit test.I would like to ask this question from Cones at Angle of Attack in division Three-Dimensional Flow of Aerodynamics
• There is a large gradient of entropy near the surface of the cone.(a) True(b) FalseI got this question in an interview for job.This is a very interesting question from Cones at Angle of Attack topic in section Three-Dimensional Flow of Aerodynamics
• What happens when the cross – flow velocity becomes supersonic?(a) Embedded shock waves on windward side(b) Embedded shock waves on the leeward side(c) Expansion shock waves on the windward side(d) Oblique shock waves on the leeward sideThe question was posed to me in my homework.This interesting question is from Cones at Angle of Attack topic in section Three-Dimensional Flow of Aerodynamics
• When does embedded shock wave appear on the cone kept at an angle?(a) Angle of attack = half cone angle(b) Angle of attack > half cone angle(c) Angle of attack < half cone angle(d) Shock wave angle = 90 degreesI have been asked this question in semester exam.Question is from Cones at Angle of Attack in chapter Three-Dimensional Flow of Aerodynamics
• For a cone at an angle of attack, what is the shock wave a function of?(a) Polar angle(b) Azimuth angle(c) Angle of attack(d) Conical ray distanceThis question was addressed to me in my homework.I want to ask this question from Cones at Angle of Attack in section Three-Dimensional Flow of Aerodynamics
• When the right – circular cone is kept at an angle of attack to the free – stream, what is it considered to be?(a) One – dimensional(b) Two – dimensional(c) Three – dimensional(d) Four – dimensionalThis question was addressed to me during an online interview.Origin of the question is Cones at Angle of Attack in section Three-Dimensional Flow of Aerodynamics
• How many variables is the flow field dependent on in case of flow over a cone at an angle of attack?(a) 1(b) 2(c) 3(d) 4The question was posed to me in an online interview.I would like to ask this question from Cones at Angle of Attack in chapter Three-Dimensional Flow of Aerodynamics
• For a supersonic flow over a right – circular cone at zero angle of attack, what are the flow properties a function of?(a) Polar angle(b) Azimuth angle(c) Mach number(d) Conical ray distanceThe question was asked in a job interview.The query is from Cones at Angle of Attack topic in section Three-Dimensional Flow of Aerodynamics
• 10 Flow over an elliptical cone at zero angle of attack, the fluid properties are a function of how many elements?(a) 1(b) 2(c) 3(d) 4I had been asked this question during an interview.My question comes from Cones at Angle of Attack in division Three-Dimensional Flow of Aerodynamics