Item Details

A Potential-Flow/Boundary Layer Method for Calculating Subsonic and Transonic Airfoil Flow With Trailing-Edge Separation

Richard W. Barnwell
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 Technical Memorandum
SuDoc Number
NAS 1.15:81850
Description
37 p. : ill. ; 27 cm.
Notes
  • "Langley Research Center."
  • "June 1981"--Cover.
  • Subject Category 02.
  • Includes bibliographical references.
Series Statement
NASA technical memorandum 81850
Technical Details
  • Access in Virgo Classic

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    a| Aerofoils x| Mathematical models.
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    a| Turbulent boundary layer x| Mathematical models.
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    a| Aerodynamics, Transonic.
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