Boundary layer transition in the leading edge region of a swept cylinder in high speed flow
By: Colin P. Coleman.
Contributors: Ames Research Center.; United States. National Aeronautics and Space Administration.
Series: NASA/TM -- 1998-112224.; NASA technical memorandum -- 112224.
Publisher: National Aeronautics and Space Administration, Ames Research Center; National Technical Information Service, distributor
Published: 1998
Place of publication: Moffett Field, Calif; Springfield, VA
Language: eng
Format: Microform
Subjects: Boundary layer transition.; Leading edges.; Wind tunnel tests.; Reynolds number.; Swept wings.; Supersonic flow.
Notes: Shipping list no.: 99-0685-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1998] 3 microfiches.