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Shock generation and control using DBD plasma actuators : SBIR phase I final report /

Bibliographic Details
Main Author: Patel, Mehul P. (Author)
Corporate Authors: Fundamental Aeronautics Program (U.S.) (sponsoring body.), United States. National Aeronautics and Space Administration (sponsoring body.)
Format: Government Document eBook
Language:English
Published: Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
Series:NASA contractor report ; NASA CR-217448.
Subjects:
Actuators.
Dielectrics.
Shock tests.
Wind tunnel tests.
Aircraft engines.
Turbulent boundary layer.
Boundary layer separation.
Supersonic inlets.
Oblique shock waves.
Online Access:https://purl.fdlp.gov/GPO/gpo32876
Description
Item Description:Title from title screen (viewed Jan. 15, 2013).
"June 2012."
"This work was sponsored by the Fundamental Aeronautics Program at the NASA Glenn Research Center."
Physical Description:1 online resource (34 pages) : color illustrations.
Bibliography:Includes bibliographical references (pages 33-34).