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

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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.
Airfoils.
Boundary layer control.
Laminar boundary layer.
Suction.
Supercritical wings.
Swept wings.
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