Low-speed, high-lift aerodynamic characteristics of slender, hypersonic accelerator-type configurations
By: Gregory M. Gatlin.
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
Series: NASA technical paper -- 2945.
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, D.C.]; [Springfield, Va
Language: eng
Format: Microform
Number of pages: 43
Subjects: Lift (Aerodynamics); Hypersonic planes.; Aerodynamic characteristics.; Aerospace planes.; Aircraft design.; Body-wing configurations.; Hypersonic flow.; Lift.
Other titles: Low speed, high lift aerodynamic characteristics of slender, hypersonic accelerator-type configurations.
Notes: Prepared at Langley Research Center.

Shipping list no.: 92-0758-M.

Includes bibliographical references (p. 8).

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/19900001514%5F1990001514.pdf; current access available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1990]. 1 microfiche.