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 /

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Bibliographic Details
Author / Creator:Wood, Richard M., author.
Imprint:Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, July 1985.
Description:1 online resource (119 pages) : illustrations.
Language:English
Series:NASA/TP ; 2433
NASA technical paper ; 2433.
Subject:
Airplanes -- Wings, Triangular -- Aerodynamics.
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/11618620
Hidden Bibliographic Details
Other authors / contributors:Covell, Peter F., author.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, issuing body.
Langley Research Center.
Notes:Includes bibliographical references (page 119).
Technical paper.
Langley Research Center 505-43-23-02 L-15899
Description based on online resource, PDF version; title from title page (NASA, viewed June 15, 2018).
Other form:Print version: Wood, Richard M 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
GPO item no.:0830-H-15 (online)
Govt.docs classification:NAS 1.60:2433

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