The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil : suction coefficient analysis /
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| Author / Creator: | Brooks, Cuyler W., Jr. |
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| Imprint: | [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; Springfield, Va. : For sale by the National Technical Information Service, 1991. |
| Description: | 18 pages : illustrations ; 28 cm. |
| Language: | English |
| Series: | NASA technical memorandum ; 4267 NASA technical memorandum ; 4267. |
| Subject: | Aerodynamics, Transonic. Aerofoils -- Testing. Boundary layer. Drag (Aerodynamics) Laminar flow. Airfoils. Boundary layer control. Laminar boundary layer. Suction. Supercritical wings. Swept wings. |
| Format: | E-Resource Microform U.S. Federal Government Document Book |
| URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/6526255 |
| Item Description: | "June 1991." Prepared at Langley Research Center. |
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| Physical Description: | 18 pages : illustrations ; 28 cm. |
| Format: | 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). |