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

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