A flight investigation of the boundary-layer characteristics and profile drag of the NACA 35-215 laminar-flow airfoil at high Reynolds numbers / by J.W. Wetmore, J.A. Zalovcik, and Robert C. Platt.

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Bibliographic Details
Main Author:	Wetmore, J. W. (Joseph W.)
Corporate Authors:	United States. National Advisory Committee for Aeronautics, Langley Aeronautical Laboratory
Other Authors:	Platt, Robert C., Zalovcik, John A.
Other title:	NACA Wartime Reports. Series L.
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : National Advisory Committee for Aeronautics, [1941]
Series:	Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L532.
Subjects:	Aerofoils. Boundary layer. Laminar flow. Drag (Aerodynamics) Charts, diagrams, etc.

Norlin Library - Basement - Government Information - US

Holdings details from Norlin Library - Basement - Government Information - US
Call Number:	Y 3.N 21/5:11/L532
Y 3.N 21/5:11/L532	Available Place a Hold