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
By: Richard M. Wood and Peter F. Covell.
Contributors: Covell, Peter F.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Series: NASA technical paper -- 2433.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service
Published: 1985
Place of publication: [Washington, D.C.]; Springfield, Va
Language: eng
Format: Microform
Subjects: Delta wings.; Supersonic airfoils.; Supersonic flow.; Sweptback wings.
Notes: Includes bibliographical references.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1985] 2 microfiches.