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 /

Bibliographic Details
Main Author: Coleman, Colin P.
Corporate Authors: Ames Research Center, United States. National Aeronautics and Space Administration
Format: Government Document Book
Language:English
Published: Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [1998]
Series:NASA technical memorandum ; 112224.
Subjects:
Boundary layer transition.
Leading edges.
Wind tunnel tests.
Reynolds number.
Swept wings.
Supersonic flow.

Evans: US Documents Microfiche (3rd floor)

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Call Number: NAS 1.15:112224
 
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NAS 1.15:112224 Available