Experimental and theoretical aerodynamic characteristics of a high-lift semispan wing model
By: Zachary T. Applin and Garl L. Gentry, Jr.
Contributors: Gentry, Garl L.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
Series: NASA technical paper -- 2990.
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division; For sale by the National Technical Information Service]
Published: 1990
Place of publication: [Washington, D.C.]; [Springfield, Va
Language: eng
Format: Microform
Number of pages: 108
Subjects: Airplanes -- Wings -- Aerodynamics.; Lift (Aerodynamics); Laminar flow.; Aerodynamic characteristics.; Aerodynamic configurations.; Airfoil profiles.; Boundary layer control.; Computer programs.; Laminar boundary flow.; Panel method (Fluid dynamics); Semispan models.
Notes: Prepared at Langley Research Center.

Includes bibliographical references (p. 21).

Also available via Internet from the NASA Technical Report Server web site. Address as of 4/10/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900010730%5F1990010730.pdf; current access available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1991]. 2 microfiches.