Boundary layer transition in the leading edge region of a swept cylinder in high speed flow

Boundary layer transition in the leading edge region of a swept cylinder in high speed flow [microform] / Colin P. Coleman.

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Bibliographic Details
Main Author: Coleman, Colin P.
Corporate Authors: Ames Research Center, United States. National Aeronautics and Space Administration
Format: Government Document Microfilm Book
Language:English
Published: Moffett Field, Calif. : Springfield, VA : National Aeronautics and Space Administration, Ames Research Center ; National Technical Information Service, distributor, [1998]
Series:NASA technical memorandum ; 112224.
Subjects:
Boundary layer transition.
Leading edges.
Wind tunnel tests.
Reynolds number.
Swept wings.
Supersonic flow.
Description
Item Description:Shipping list number: 99-0685-M.
Physical Description:1 volume.
Reproduction Note:Microfiche.

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