For the case in Prob. 17.1, calculate the boundary-layer thickness at the trailing edge for (a) Completely

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For the case in Prob. 17.1, calculate the boundary-layer thickness at the trailing edge for

(a) Completely laminar flow

(b) Completely turbulent flow

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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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For the case in Prob. 17.1, calculate the boundary-layer thickness at the trailing edge for (a) Completely

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A B 50x 501...View the full answer

Fundamentals of Aerodynamics

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