Air flows through the test section of a small wind tunnel at speed V = 7.5 ft/s. The temperature of
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Air flows through the test section of a small wind tunnel at speed V = 7.5 ft/s. The temperature of the air is 80°F, and the length of the wind tunnel test section is 1.5 ft. Assume that the boundary layer thickness is negligible prior to the start of the test section. Is the boundary layer along the test section wall laminar or turbulent or transitional?
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Related Book For
Fluid Mechanics Fundamentals And Applications
ISBN: 9780073380322
3rd Edition
Authors: Yunus Cengel, John Cimbala
Question Details
Chapter #
10- APPROXIMATE SOLUTIONS OF THE NAVIER–STOKES EQUATION
Section: Problems
Problem: 86
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Question Posted: September 17, 2023 00:43:53