Drag measurements at high Reynolds numbers of a 100-inch-chord NACA 23016 practical construction wing section submitted by Chance Vought Aircraft Company /

Drag measurements at high Reynolds numbers of a 100-inch-chord NACA 23016 practical construction wing section submitted by Chance Vought Aircraft Company / by Albert E. von Doenhoff and Robert J. Nuber.

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Calculation of the high-speed performance of some airplanes involves the estimation of airfoil drag coefficients at Reynolds numbers of the order of 65 to 75 million. Very little data on airfoil drag coefficients at such high Reynolds numbers are available. Drag measurements were made in the Langley...

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Bibliographic Details
Main Author: Von Doenhoff, Albert E.
Corporate Authors: United States. National Advisory Committee for Aeronautics, Langley Aeronautical Laboratory
Other Authors: Nuber, Robert J.
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. L752.
Subjects:
Airplanes > Wings.
Airplanes > Models > Testing.
Aerofoils > Testing.
Reynolds number.
Drag (Aerodynamics)
Wind tunnel testing.
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/L752
Y 3.N 21/5:11/L752 Available Place a Hold

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