Experimental and theoretical study of the longitudinal aerodynamic characteristics of delta and double-delta wings at mach numbers of 1.60, 1.90, and 2.16 /

Experimental and theoretical study of the longitudinal aerodynamic characteristics of delta and double-delta wings at mach numbers of 1.60, 1.90, and 2.16 /

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Bibliographic Details
Main Authors: Wood, Richard M. (Author), Covell, Peter F. (Author)
Corporate Author: Langley Research Center
Format: Government Document Electronic eBook
Language:English
Published: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, July 1985.
Series:NASA technical paper ; 2433.
Subjects:
Delta wings.
Supersonic airfoils.
Mach number.
Sweptback wings.
Supersonic flow.
Online Access:CONNECT
Description
Item Description:"July 1985."
Physical Description:1 online resource (119 pages, 1 unnumbered page) : illustrations.
Bibliography:Includes bibliographical references (page 119).

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