Cover Image

Flight demonstration of a shock location sensor using constant voltage hot-film anemometry /

Bibliographic Details
Main Authors: Moes, Timothy R. (Author), Sarma, Garimella R. (Author), Mangalam, Siva M. (Author)
Corporate Authors: NASA Dryden Flight Research Center, United States. National Aeronautics and Space Administration (sponsoring body.)
Format: Government Document eBook
Language:English
Published: [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, August 1997.
Series:NASA technical memorandum ; 4806.
Subjects:
Transonic speed.
Leading edges.
Laminar boundary layer.
Hot-film anemometers.
Airfoils.
Online Access:https://purl.fdlp.gov/GPO/gpo66599
Description
Item Description:Title from title screen (viewed March 30, 2016).
"August 1997."
"Performing organization: NASA Dryden Flight Research Center, Edwards, California"--Report documentation page.
Physical Description:1 online resource (25 pages) : illustrations.
Bibliography:Includes bibliographical references (page 25).