For a supersonic flow over a right – circular cone at zero angle of – McqOptions

MCQOPTIONS

1.	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 distance
Answer» B. Azimuth angle

Discussion

No Comment Found

Related MCQs

When does embedded shock wave appear on the cone kept at an angle?
What happens when the cross – flow velocity becomes supersonic?
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 = 1b) Vθ + Vϕ = 0c) Vθ2 + Vϕ2 = 0d) (Vθ + Vϕ)2 = 1 10 Flow over an elliptical cone at zero angle of attack, the fluid properties are a function of how many elements?
There is a large gradient of entropy near the surface of the cone.
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?
Vortical singularity exists at which part of the conical surface?
For a cone at an angle of attack, what is the shock wave a function of?
Streamlines curl from the leeward to the windward surface along the conical surface when kept at an angle to the free stream.
How many variables is the flow field dependent on in case of flow over a cone at an angle of attack?
When the right – circular cone is kept at an angle of attack to the free – stream, what is it considered to be?