An edition of A potential-flow/boundary layer method for calculating subsonic and transonic airfoil flow with trailing-edge separation (1981)

A potential-flow/boundary layer method for calculating subsonic and transonic airfoil flow with trailing-edge separation

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A potential-flow/boundary layer method for ca ...
Richard W. Barnwell, Richard W ...
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Last edited by WorkBot
December 15, 2009 | History
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An edition of A potential-flow/boundary layer method for calculating subsonic and transonic airfoil flow with trailing-edge separation (1981)

A potential-flow/boundary layer method for calculating subsonic and transonic airfoil flow with trailing-edge separation

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Publish Date
Publisher
National Aeronautics and Space Administration, Scientific and Technical Information Branch, For sale by the National Technical Information Service]
Language
English
Pages
37

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Subjects

Aerodynamics, Transonic, Aerofoils, Mathematical models, Transonic Aerodynamics, Turbulent boundary layer

Places

Mathematical models

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Edition Availability
Cover of: A potential-flow/boundary layer method for calculating subsonic and transonic airfoil flow with trailing-edge separation
A potential-flow/boundary layer method for calculating subsonic and transonic airfoil flow with trailing-edge separation
1981, National Aeronautics and Space Administration, Scientific and Technical Information Branch, For sale by the National Technical Information Service]
in English
Cover of: A potential-flow/boundary layer method for calculating subsonic and transonic airfoil flow with trailing-edge separation
A potential-flow/boundary layer method for calculating subsonic and transonic airfoil flow with trailing-edge separation
1981, National Aeronautics and Space Administration, Scientific and Technical Information Branch, For sale by the National Technical Information Service]
in English
Cover of: A potential-flow/boundary layer method for calculating subsonic and transonic airfoil flow with trailing-edge separation
A potential-flow/boundary layer method for calculating subsonic and transonic airfoil flow with trailing-edge separation
1981, National Aeronautics and Space Administration, Scientific and Technical Information Branch, For sale by the National Technical Information Service]
in English
  • Not in Library

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Book Details

Edition Notes

"Langley Research Center."

"June 1981"--Cover.

Subject Category 02.

Includes bibliographical references.

Published in
Washington, D.C, [Springfield, Va
Series
NASA technical memorandum -- 81850.

The Physical Object

Pagination
37 p. :
Number of pages
37

ID Numbers

Open Library
OL17123096M

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History

Download catalog record: RDF / JSON / OPDS | Wikipedia citation
December 15, 2009 Edited by WorkBot link works
September 27, 2008 Created by ImportBot Imported from Oregon Libraries MARC record