Flight investigation of boundary-layer control by suction slots on an NACA 35-215 low-drag airfoil at high Reynolds numbers /

Flight investigation of boundary-layer control by suction slots on an NACA 35-215 low-drag airfoil at high Reynolds numbers / by John A. Zalovcik, J.W. Wetmore, and Albert E. von Doenhoff.

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An investigation of the effectiveness of suction slots as a means of extending the laminar boundary layer has been made in flight at Reynolds numbers on an NACA 35-215 airfoil. The test panel, having a chord of 204 inches and an average span of 90 inches, was mounted on the left wing of a Douglas B-...

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Bibliographic Details
Main Author: Zalovcik, John A.
Corporate Authors: United States. National Advisory Committee for Aeronautics, Langley Aeronautical Laboratory
Other Authors: Wetmore, J. W. (Joseph W.), Von Doenhoff, Albert E.
Other title:NACA Wartime Reports. Series L.
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, [1944]
Series:Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L521.
Subjects:
Airplanes > Wings.
Aerofoils.
Boundary layer control.
Drag (Aerodynamics)
Aerodynamic load.
Airplanes > Flight testing.
Yawing (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/L521
Y 3.N 21/5:11/L521 Available Place a Hold

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