The NASA Langley laminar-flow-control experiment on a swept supercritical airfoil
Subtitle: basic results for slotted configuration
By: Charles D. Harris ... [et al.].
Contributors: Harris, Charles D., 1952-; United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
Series: NASA technical memorandum -- 4100.
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division; For sale by the National Technical Information Service]
Published: 1989
Place of publication: [Washington, DC]; [Springfield, Va
Language: eng
Format: Microform
Number of pages: 118
Subjects: Drag (Aerodynamics); Laminar flow.; Aerofoils -- Aerodynamics.; Airplanes -- Wings, Swept-back -- Aerodynamics.; Boundary layer control.; Laminar flow.; Supercritical airfoils.; Swept wings.; Transonic flow.; Wing slots.
Other titles: NASA Langley laminar flow control experiment on a swept supercritical airfoil.
Notes: Distributed to depository libraries in microfiche.

Includes bibliographical references (p. 14-15).

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1989] 2 microfiches : negative.