The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil : suction coefficient analysis /

Saved in:

Bibliographic Details
Author / Creator:	Brooks, Cuyler W., Jr.
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:	18 pages : illustrations ; 28 cm.
Language:	English
Series:	NASA technical memorandum ; 4267 NASA technical memorandum ; 4267.
Subject:	Aerodynamics, Transonic. Aerofoils -- Testing. Boundary layer. Drag (Aerodynamics) Laminar flow.
Format:	E-Resource Microform U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/6526255

Hidden Bibliographic Details
Varying Form of Title:	Suction coefficient analysis
Other authors / contributors:	Harris, Charles D., 1952- Harvey, William D., 1934- United States. National Aeronautics and Space Administration. Scientific and Technical Information Program. Langley Research Center.
Notes:	"June 1991." Prepared at Langley Research Center. Includes bibliographical references (page 7). Available via Internet from the NTRS web site. Address as of 1/18/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19910014785%5F1991014785.pdf; current access is available via PURL.
GPO item no.:	0830-D (MF) 0830-D (online)
Govt.docs classification:	NAS 1.15:4267

Similar Items