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For an incompressible plane flow in polar coordinates (r plane) we have an expression for the radial velocity component given by, vr=r3cos+r2sin. Determine an expression

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For an incompressible plane flow in polar coordinates (r plane) we have an expression for the radial velocity component given by, vr=r3cos+r2sin. Determine an expression for the circumferential velocity profile, v, that satisfies continuity

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