Experimental investigation of the pressure distribution about a yawed circular cylinder in the critical Reynolds number range

William J. Bursnall, Lawrence K. Loftin, Jr.
Sep 1951

An experimental investigation has been made of the pressure distribution about a circular cylinder at yaw angles of 0, 15, 30, 45, and 60 degrees for Reynolds numbers from below the critical value up to about 5.0 X 10(exp 5).

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