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

William J. Bursnall, Lawrence K. Loftin, Jr.
naca-tn-2463
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).

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1951/naca-tn-2463.pdf