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Author Coe, Paul L., author.

Title Leading-edge deflection optimization for a highly swept arrow-wing configuration / Paul L. Coe, Jr., Jarrett K. Huffman, and James W. Fenbert.

Publication Info. [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.

Copies

Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.60:1777    ---  Available
Description 1 online resource (56 pages) : illustrations.
text txt rdacontent
computer c rdamedia
online resource cr rdacarrier
Series NASA technical paper ; 1777
NASA technical paper ; 1777.
Note Title from title screen (viewed on Aug. 25, 2016).
"December 1980."
"Performing Organization: NASA Langley Research Center"--Report documentation page.
Bibliography Includes bibliographical references (pages 55-56).
Type Of Report Technical paper.
Funding National Aeronautics and Space Administration 533-01-43-02 L-13820
Subject Aerodynamics.
Airplanes -- Wings, Swept-back.
Leading edges (Aerodynamics)
Aerodynamics. (OCoLC)fst00798195
Airplanes -- Wings, Swept-back. (OCoLC)fst00803560
Leading edges (Aerodynamics) (OCoLC)fst00994749
Genre/Form Online resources.
Electronic books.
Electronic government information.
Added Author Huffman, Jarrett K., author.
Fenbert, James W., author.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, issuing body.
Other Form: Print version: Coe, Paul L. Leading-edge deflection optimization for a highly swept arrow-wing configuration (OCoLC)7503108
Microfiche version: Coe, Paul L. Leading-edge deflection optimization for a highly swept arrow-wing configuration (OCoLC)711544844
Gpo Item No. 0830-H-15 (online)
Sudoc No. NAS 1.60:1777

 
    
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