Flight demonstration of a shock location sensor using constant voltage hot-film anemometry
By: Timothy R. Moes, Garimella R. Sarma and Siva M. Mangalam.
Contributors: Sarma, Garimella R.; Mangalam, Siva M.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Program.
Series: NASA technical memorandum -- 4806.
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program; National Technical Information Service, distributor]
Published: 1997
Place of publication: [Washington, D.C.]; [Springfield, Va
Language: eng
Format: Microform
Subjects: F-15 aircraft.; Transonic speed.; Pressure sensors.; Leading edges.; Laminar boundary layer.; Hot-film anemometers.; Airfoils.
Notes: Shipping list no.: 98-0799-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.