A study of the leading edge of a shock induced boundary layer /

Bibliographic Details
Main Author:	Sichel, Martin
Corporate Authors:	Princeton University. Department of Aeronautical Engineering, United States. Air Force. Air Research and Development Command
Format:	Book
Language:	English
Published:	[Princeton, N.J.] : Princeton University Dept. of Aeronautical Engineering, [1961]
Series:	Report (Princeton University. Department of Aeronautical Engineering) ; 540.
Subjects:	Boundary layer > Mathemataical models. Laminar flow > Mathematical models. Aeronautics > Research > United States. Shock waves > Mathematical models.

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