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Title	Leading-edge deflection optimization for a highly swept arrow-wing configuration /
Format	online resource
Internet Access	https://purl.fdlp.gov/GPO/gpo71426
Author	Coe, Paul L., author.
Published	[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.

SuDoc Number	NAS 1.60:1777
Item Number	0830-H-15 (online)
Description	1 online resource (56 pages) : illustrations.
Content Type	text
Series	(NASA technical paper ; 1777.)
General 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).
Added Entry	Huffman, Jarrett K., author.
	Fenbert, James W., author.
Added Entry	Langley Research Center.
	United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, issuing body.
Linking Field	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
URL	http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19810006459.pdf

Holdings	All items

OCLC Number	(OCoLC)760918532
CGP Record Link	https://catalog.gpo.gov:443/F/?func=direct&doc_number=000992680&local_base=GPO01PUB
System Number	000992680