Effect of chordwise location of maximum thickness on the supersonic wave drag of sweptback wings /

Effect of chordwise location of maximum thickness on the supersonic wave drag of sweptback wings / Kenneth Margolis.

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Bibliographic Details
Main Author: Margolis, Kenneth
Corporate Author: United States. National Advisory Committee for Aeronautics
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) ; 1543.
Subjects:
Airplanes > Wings, Swept-back.
Drag (Aerodynamics)
Aerodynamics, Supersonic.
Description
Item Description:"March 1948."
NACA TN Number 1543.
Physical Description:30 pages : illustrations ; 28 cm.
Bibliography:Includes bibliographical references.
Action Note:committed to retain

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