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For a source flow, show that it is a physically possible incompressible flow except at origin. Also, show that it …
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Show that a uniform flow with velocity \({V_\infty }\) is a physically possible incompressible flow and is irrotational.
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Prove that velocity potential and stream function for a uniform flow and source flow satisfies Laplace’s equation.
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If the velocity \({V_\infty }\) of a flow is doubled in the case of lifting flow over a circular cylinder of …
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Calculate the lift per unit span for a lifting flow over a circular cylinder with a diameter of 0.8 m, …
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Calculate the peak coefficient of pressure for a lifting flow over a circular cylinder for which lifting coefficient is 7.
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Consider the non lifting flow over a circular cylinder of a given radius, where free stream velocity is \({V_\infty }\).If \({V_\infty …
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Consider a non-lifting flow over a circular cylinder and derive an expression for the pressure coefficient at any arbitrary point …
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Calculate locations on the surface of a cylinder where surface pressure equals to free-stream pressure considering a non-lifting flow.
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Lift per unit span of a spinning circular cylinder in a free stream with velocity of 50 m/s is 8 …
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- 1 answers
- 0 votes
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