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Experimental Effects of Fuselage Camber on Longitudinal Aerodynamic Characteristics of a Series of Wing-Fuselage Configurations at a Mach of 1.41

Samuel M. Dollyhigh, Odell A. Morris, and Mary S. Adams ; Langley Research Center, Hampton, Va
Format
Book; Government Document
Published
Washington : U.S. National Aeronautics and Space Administration ; Springfield, Va. : for sale by the National Technical Information Service, 1976.
Language
English
Series
NASA technical memorandum
Description
[1], 25 p. : ill. ; 27 cm.
Notes
  • Cover title.
  • Bibliography: p. 14.
Series Statement
NASA technical memorandum NASA TM X-3411
Technical Details
  • Access in Virgo Classic
  • Staff View

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