Item Details

Effect of Canard Leading-Edge Sweep and Dihedral Angle on the Longitudinal and Lateral Aerodynamic Characteristics of a Close-Coupled Canard-Wing Configuration

by Blair B. Gloss
Format
Book; Government Document; Online; EBook
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974.
Language
English
Series
NASA Technical Note
Description
68 p. : ill. ; 27 cm.
Mode of access: Internet.
Notes
  • Prepared at Langley Research Center.
  • Cover title.
  • Includes bibliographical references (p. 12-13).
Series Statement
NASA technical note ; NASA TN D-7814
Logo for No Copyright - United StatesNo Copyright - United States
Technical Details

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    a| Effect of canard leading-edge sweep and dihedral angle on the longitudinal and lateral aerodynamic characteristics of a close-coupled canard-wing configuration / c| by Blair B. Gloss.
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    a| Washington, D.C. : b| National Aeronautics and Space Administration ; a| [Springfield, Va. : b| For sale by the National Technical Information Service], c| 1974.
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    a| 68 p. : b| ill. ; c| 27 cm.
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    a| NASA technical note ; v| NASA TN D-7814
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    a| Prepared at Langley Research Center.
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    a| Cover title.
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    a| Includes bibliographical references (p. 12-13).
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    a| Mode of access: Internet.
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    a| Stability of airplanes, Lateral.
    650
      
    0
    a| Stability of airplanes, Longitudinal.
    650
      
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    a| Leading edges (Aerodynamics)
    650
      
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    a| Airplanes x| Wings, Canard.
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