Boundary-layer development and skin friction at Mach number 3.05 / Paul F. Brinich and Nick S. Diaconis.

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Bibliographic Details
Main Author:	Brinich, Paul F.
Corporate Author:	United States. National Advisory Committee for Aeronautics
Other Authors:	Diaconis, Nick S.
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : National Advisory Committee for Aeronautics, 1952.
Series:	Technical note (United States. National Advisory Committee for Aeronautics) ; 2742.
Subjects:	Boundary layer. Turbulent boundary layer. Air flow. Skin friction (Aerodynamics) Mach number. Aerodynamics, Supersonic.

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Call Number:	Y 3.N 21/5:6/2742
Y 3.N 21/5:6/2742	Available Place a Hold