Dynamic ground-effect measurements on the F-15 STOL and Maneuver Technology Demonstrator (S/MTD) configuration
By: Guy T. Kemmerly.
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.; Langley Research Center.
Series: NASA technical paper -- 3000.
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: 28
Subjects: Aerodynamic characteristics.; Aircraft configurations.; Aircraft landing.; F-15 aircraft.; Ground effect (Aerodynamics); Ground tests.; Short takeoff aircraft.
Notes: Shipping list no.: 1991-0132-M.

Distributed to depository libraries in microfiche.

Prepared at Langley Research Center.

Bibliography: p. 12.

Also available via Internet from the NTRS web site. Address as of 3/23/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900013215%5F1990013215.pdf; current access is available via PURL.

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