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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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    a| GPO c| GPO d| MvI-ran d| MvI-ran
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    a| NAS 1.15:X-3411
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    1
      
    a| Dollyhigh, Samuel M.
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    1
    0
    a| Experimental effects of fuselage camber on longitudinal aerodynamic characteristics of a series of wing-fuselage configurations at a mach of 1.41 / c| Samuel M. Dollyhigh, Odell A. Morris, and Mary S. Adams ; Langley Research Center, Hampton, Va.
    260
      
      
    a| Washington : b| U.S. National Aeronautics and Space Administration ; a| Springfield, Va. : b| for sale by the National Technical Information Service, c| 1976.
    300
      
      
    a| [1], 25 p. : b| ill. ; c| 27 cm.
    440
      
    0
    a| NASA technical memorandum v| NASA TM X-3411.
    500
      
      
    a| Cover title.
    504
      
      
    a| Bibliography: p. 14.
    596
      
      
    a| 14
    650
      
    0
    a| Airplanes x| Fuselage.
    650
      
    0
    a| Airplanes x| Design and construction.
    700
    1
      
    a| Morris, Odell A., e| jt. auth.
    700
    1
      
    a| Adams, Mary S., e| jt. auth.
    710
    2
      
    a| Langley Research Center.
    710
    1
      
    a| United States. b| National Aeronautics and Space Administration.
    999
      
      
    a| Readex MicPrnt 77-788 w| SUDOC i| 1392853-1001 l| BY-REQUEST m| IVY t| BOOK
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