Aerospace Engineering > GATE 2025 > Potential Flow
The lift per unit span for a spinning circular cylinder in a potential flow is 6 N/m. The free-stream velocity is 30 m/s, and the density of air is 1.225 kg/m3. The circulation around the cylinder is ______ m2/s (rounded off to two decimal places).

Correct : 0.16

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lift per unit span cylinder GATE Aerospace Engineering 2025 spinning cylinder lift potential flow lift free stream velocity air density circulation around cylinder GATE aerospace lift cylinder calculation

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