Consider the non-lifting flow over a circular cylinder. Derive an expression for the pressure coefficient at an

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Consider the non-lifting flow over a circular cylinder. Derive an expression for the pressure coefficient at an arbitrary point (r, θ) in this flow, and show that it reduces to Eq. (3.101) on the surface of the cylinder.

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Fundamentals of Aerodynamics

ISBN: 978-0070016798

2nd Edition

Authors: J. Anderson

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Question Posted: Dec 09, 2010 03:24 AM

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Consider the non-lifting flow over a circular cylinder. Derive an expression for the pressure coefficient at an

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r Ve v 11 11 11 1 a rae Vor sine 1 ...View the full answer

Fundamentals of Aerodynamics

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