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Calculation of Vortex Lift Effect for Cambered Wings by the Suction Analogy

C. Edward Lan and Jen-Fu Chang ; prepared for Langley Research Center under grant NSG-1629
Format
Book; Government Document
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981.
Language
English
Series
NASA Contractor Report
SuDoc Number
NAS 1.26:3449
Description
83 p. : ill. ; 28 cm.
Notes
  • "The University of Kansas Center for Research, Inc."
  • "July 1981"--Cover.
  • Includes bibliographical references.
Series Statement
NASA contractor report 3449
Technical Details
  • Access in Virgo Classic
  • Staff View

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    a| Washington, D.C. : b| National Aeronautics and Space Administration, Scientific and Technical Information Branch ; a| [Springfield, Va. : b| For sale by the National Technical Information Service], c| 1981.
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    a| Includes bibliographical references.
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    a| Lift (Aerodynamics)
    650
      
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    a| Camber (Aerofoils)
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