Investigation of boundary-layer Reynolds number for transition on an NACA 65₍₂₁₅₎-114 airfoil in the Langley two-dimensional low-turbulence pressure tunnel / Albert L. Braslow and Fioravante Visconti.

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Bibliographic Details
Main Author:	Braslow, Albert L.
Corporate Author:	United States. National Advisory Committee for Aeronautics
Other Authors:	Visconti, Fioravante
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : National Advisory Committee for Aeronautics, 1948.
Series:	Technical note (United States. National Advisory Committee for Aeronautics) ; 1704.
Subjects:	Aerofoils. Boundary layer. Laminar flow. Turbulence. Reynolds number. Wind tunnel testing.

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Call Number:	Y 3.N 21/5:6/1704
Y 3.N 21/5:6/1704	Available Place a Hold