The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil
Subtitle: suction coefficient analysis
By: Cuyler W. Brooks, Jr., Charles D. Harris, and William D. Harvey.
Contributors: Harris, Charles D., 1952-; Harvey, William D., 1934-; United States. National Aeronautics and Space Administration. Scientific and Technical Information Program.; Langley Research Center.
Series: NASA technical memorandum -- 4267.
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program; For sale by the National Technical Information Service
Published: 1991
Place of publication: [Washington, D.C.]; Springfield, Va
Language: eng
Format: Microform
Number of pages: 18
Subjects: Aerodynamics, Transonic.; Aerofoils -- Testing.; Boundary layer.; Drag (Aerodynamics); Laminar flow.; Airfoils.; Boundary layer control.; Laminar boundary layer.; Suction.; Supercritical wings.; Swept wings.
Other titles: Suction coefficient analysis.
Notes: "June 1991."

Prepared at Langley Research Center.

Includes bibliographical references (p. 7).

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.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration,] 1991. 1 microfiche : negative.