Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil /

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Bibliographic Details
Author / Creator:	Hahne, David E. (David Edgar)
Imprint:	[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; Springfield, Va. : For sale by the National Technical Information Service, 1991.
Description:	48 pages : illustrations ; 28 cm.
Language:	English
Series:	NASA technical paper ; 3133 NASA technical paper ; 3133.
Subject:	Aerofoils -- Testing. Airplanes -- Wings -- Testing. Laminar flow. Airfoil profiles. Flapping. Full scale tests. Jet aircraft. Laminar flow airfoils. Low speed. Semispan models. Wind tunnel tests.
Format:	E-Resource Microform U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/6508772

Hidden Bibliographic Details
Other authors / contributors:	Jordan, Frank L. United States. National Aeronautics and Space Administration. Scientific and Technical Information Program. Langley Research Center.
Notes:	"September 1991." Prepared at Langley Research Center. Bibliography: pages 6-7. Available via Internet from the NTRS web site. Address as of 3/16/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19910020784%5F1991020784.pdf; current access is available via PURL.
GPO item no.:	0830-H-15 (MF) 0830-H-15 (online)
Govt.docs classification:	NAS 1.60:3133

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