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Theoretical and Experimental Study of Twisted and Cambered Delta Wings Designed for a Mach Number of 3.5

Russell B. Sorrells III, and Emma Jean Landrum ; Langley Research Center, Hampton, Va
Format
Book; Government Document
Published
Washington : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the National Technical Information Service, 1976.
Language
English
Series
NASA Technical Note
Description
236 p. : ill. ; 27 cm.
Notes
  • Cover title.
  • Bibliography: p. 13.
Series Statement
NASA technical note NASA TN D-8247
Technical Details
  • Access in Virgo Classic
  • Staff View

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    a| Sorrells, Russell B.
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    0
    a| Theoretical and experimental study of twisted and cambered delta wings designed for a Mach number of 3.5 / c| Russell B. Sorrells III, and Emma Jean Landrum ; Langley Research Center, Hampton, Va.
    260
      
      
    a| Washington : b| National Aeronautics and Space Administration ; a| Springfield, Va. : b| for sale by the National Technical Information Service, c| 1976.
    300
      
      
    a| 236 p. : b| ill. ; c| 27 cm.
    440
      
    0
    a| NASA technical note v| NASA TN D-8247.
    500
      
      
    a| Cover title.
    504
      
      
    a| Bibliography: p. 13.
    596
      
      
    a| 14
    650
      
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    a| Aerodynamic load.
    650
      
    0
    a| Airplanes x| Wings.
    700
    1
      
    a| Landrum, Emma J., e| jt. auth.
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    a| United States. b| National Aeronautics and Space Administration.
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    a| Langley Research Center.
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