Item Details

Influence of Airfoil Geometry on Delta Wing Leading-Edge Vortices and Vortex-Induced Aerodynamics at Supersonic Speeds

Richard M. Wood, James E. Byrd, and Gary F. Wesselmann
Format
Book; Government Document; Online; EBook
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.
Language
English
Series
NASA Technical Paper
Description
v, 77 p. : ill. ; 28 cm.
Mode of access: Internet.
Notes
  • Prepared at Langley Research Center.
  • Includes bibliographical references (p. 6).
Series Statement
NASA technical paper ; 3105
Logo for Copyright Not EvaluatedCopyright Not Evaluated
Technical Details

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    a| Influence of airfoil geometry on delta wing leading-edge vortices and vortex-induced aerodynamics at supersonic speeds / c| Richard M. Wood, James E. Byrd, and Gary F. Wesselmann.
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    a| Washington, D.C. : b| National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, c| 1992.
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    a| v, 77 p. : b| ill. ; c| 28 cm.
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    a| NASA technical paper ; v| 3105
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    a| Prepared at Langley Research Center.
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    a| Includes bibliographical references (p. 6).
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    a| Mode of access: Internet.
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    6
    a| Aérodynamique supersonique.
    650
      
    6
    a| Tourbillons (Mécanique des fluides)
    650
      
    6
    a| Bords d'attaque (Aérodynamique)
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    a| Avions x| Ailes delta.
    650
      
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    a| Aerodynamics, Supersonic.
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    a| Vortex-motion.
    650
      
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    a| Leading edges (Aerodynamics)
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    a| Airplanes x| Wings, Triangular.
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    a| Wesselmann, Gary F.
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    a| Byrd, James E.
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    a| Langley Research Center.
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    b| UIU c| UIUC d| 20141113 s| google u| uiug.30112106710905 y| 1992 r| pd q| bib

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