Leading-edge deflection optimization for a highly swept arrow-wing configuration

Leading-edge deflection optimization for a hi ...
Paul L. Coe, Paul L. Coe
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Last edited by WorkBot
January 19, 2010 | History

Leading-edge deflection optimization for a highly swept arrow-wing configuration

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Cover of: Leading-edge deflection optimization for a highly swept arrow-wing configuration
Leading-edge deflection optimization for a highly swept arrow-wing configuration
1980, National Aeronautics and Space Administration, Scientific and Technical Information Branch
in English
Cover of: Leading-edge deflection optimization for a highly swept arrow-wing configuration
Leading-edge deflection optimization for a highly swept arrow-wing configuration
1980, National Aeronautics and Space Administration, Scientific and Technical Information Branch
in English
Cover of: Leading-edge deflection optimization for a highly swept arrow-wing configuration
Leading-edge deflection optimization for a highly swept arrow-wing configuration
1980, National Aeronautics and Space Administration, Scientific and Technical Information Branch
in English

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Book Details


Edition Notes

"Langely Research Center, Hampton, Virginia."

Dec. 1980.

Includes bibliographial references.

Published in
Washington, D.C, [Springfield, Va. : For sale by the National Technical Information Service]
Series
NASA technical paper -- 1777.

The Physical Object

Pagination
56 p. :
Number of pages
56

Edition Identifiers

Open Library
OL17542344M

Work Identifiers

Work ID
OL11104211W

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History

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January 19, 2010 Edited by WorkBot add subjects and covers
December 11, 2009 Created by WorkBot add works page