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Consider an airfoil in a wind tunnel (i.e., a wing that spans the entire test section). Prove that the lift …
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Consider a body of arbitrary shape. If the pressure distribution over the surface of the body is constant, prove that …
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Assuming the velocity field given as u = cx and v = −cy, where c is a constant pertains to …
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Consider a flow field in polar coordinates, where the stream function is given as ψ = ψ(r, θ). Starting with …
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Consider a length of pipe bent into a U-shape. The inside diameter of the pipe is 0.5\;m. Air enters one …
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Consider a velocity field where the radial and tangential components of velocity are V_{r} = 0 and V_{θ} = cr, …
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For vortex flow, calculate: a. The time rate of change of the volume of a fluid element per unit volume. …
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For source flow, calculate: a. The time rate of change of the volume of a fluid element per unit volume. …
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Consider a velocity field where the x and y components of velocity are given by u = cx and \(v …
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Consider a velocity field where the radial and tangential components of velocity are V_{r} = 0 and V_{θ} = cr, …
- 2K views
- 1 answers
- 0 votes