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.

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number:	NAS 1.15:112224
NAS 1.15:112224	Restricted Place a Hold