Experimental and theoretical study of 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 longitudinal aerodynamic characteristics of delta and double-delta wings at Mach numbers of 1.60, 1.90, and 2.16 / Richard M. Wood and Peter F. Covell.

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Bibliographic Details
Online Access: Online Access
Main Authors: Wood, Richard M. (Author), Covell, Peter F. (Author)
Corporate Author: Langley Research Center
Format: Government Document 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:
Airplanes > Wings, Triangular > Aerodynamics.
Supersonic airfoils.
Delta wings.
Supersonic flow.
Aerodynamic drag.
Mach number.

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Call Number: NAS 1.60:2433
NAS 1.60:2433 Available

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