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

System Under Maintenance

Our Library Management System is currently under maintenance.

Holdings and item availability information is currently unavailable. Please accept our apologies for any inconvenience this may cause and contact us for further assistance:

catalog@lib.uchicago.edu

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

System Under Maintenance

Similar Items