Aerospace Engineering > GATE 2010 > Potential Flow
Consider a potential flow over a spinning cylinder.
The stream function is given as:
ψ = (V∞ r sin θ) (1 − R²/r²) + (Γ/2π) ln(r/R)
The stagnation points are located at
ψ = (V∞ r sin θ) (1 − R²/r²) + (Γ/2π) ln(r/R)
Correct : a
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