Right option is (c) Vθ^2 + Vϕ^2 = 0
Explanation: While working with three – dimensional flow over a cone kept at an angle of attack with the free stream, we look at the cross – flow plane to analyze the streamlines. The velocity on this plane is called cross – flow velocity. Stagnation point on the cone is situated where the condition Vθ^2 + Vϕ^2 = 0 is met.
In the figure, the shaded portion is the x – y plane of the cone with the outer black boundary being the shock wave. The blue lines are the streamlines with different entropies. Point A is the vortical singularity and point S is the stagnation point.