Drag reduction by suction of the boundary layer separated behind shock wave formation at high Mach numbers / by B. Regenscheit.

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Bibliographic Details
Main Author:	Regenscheit, B.
Corporate Author:	United States. National Advisory Committee for Aeronautics
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : National Advisory Commitee for Aeronautics, [1947]
Series:	Technical memorandum (United States. National Advisory Committee for Aeronautics) ; no. 1168.
Subjects:	Boundary layer. Shock waves. Drag (Aerodynamics)

Norlin Library - Basement - Government Information - US

Holdings details from Norlin Library - Basement - Government Information - US
Call Number:	Y 3.N 21/5:8/1168
Y 3.N 21/5:8/1168	Available Place a Hold