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

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Bibliographic Details
Author / Creator:	Coe, Paul L., author.
Imprint:	[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.
Description:	1 online resource (56 pages) : illustrations.
Language:	English
Series:	NASA technical paper ; 1777 NASA technical paper ; 1777.
Subject:	Aerodynamics. Airplanes -- Wings, Swept-back. Leading edges (Aerodynamics)
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/10914234

Hidden Bibliographic Details
Other authors / contributors:	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.
Notes:	Title from title screen (viewed on Aug. 25, 2016). "December 1980." "Performing Organization: NASA Langley Research Center"--Report documentation page. Includes bibliographical references (pages 55-56). Technical paper. National Aeronautics and Space Administration 533-01-43-02 L-13820
Other form:	Print version: Coe, Paul L. Leading-edge deflection optimization for a highly swept arrow-wing configuration Microfiche version: Coe, Paul L. Leading-edge deflection optimization for a highly swept arrow-wing configuration
GPO item no.:	0830-H-15 (online)
Govt.docs classification:	NAS 1.60:1777

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