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

Bibliographic Details
Main Author: Brooks, Cuyler W., Jr
Corporate Authors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Program, Langley Research Center
Other Authors: Harris, Charles D., 1952-, Harvey, William D., 1934-
Format: Government Document Microform Book
Language:English
Published: [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; 1991.
Series:NASA technical memorandum ; 4267.
Subjects:
Aerodynamics, Transonic.
Aerofoils > Testing.
Boundary layer.
Drag (Aerodynamics)
Laminar flow.
Airfoils.
Boundary layer control.
Laminar boundary layer.
Suction.
Supercritical wings.
Swept wings.
Online Access:https://purl.fdlp.gov/GPO/LPS66394
Description
Item Description:"June 1991."
Prepared at Langley Research Center.
Microform.
Physical Description:18 pages : illustrations ; 28 cm.
Also 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.
Bibliography:Includes bibliographical references (page 7).