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DBD plasma actuators for flow control in air vehicles and jet engines : simulation of flight conditions in test chambers by density matching /

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Bibliographic Details
Main Authors: Ashpis, D. E. (David E.) (Author), Thurman, Douglas R. (Author)
Corporate Authors: United States. National Aeronautics and Space Administration (sponsoring body.), U.S. Army Research Laboratory (sponsoring body.)
Format: Government Document eBook
Language:English
Published: Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2011.
Edition:[Revised].
Series:NASA technical memorandum ; 2011-217006/REV 1.
Subjects:
Jet engines.
Actuators.
Active control.
Dielectrics.
Gas density.
Turbines.
Pressure distribution.
Plasma jets.
Magnetohydrodynamic flow.
Online Access:https://purl.fdlp.gov/GPO/gpo45706
Description
Item Description:Title from title screen (viewed on Feb. 4, 2014).
"July 2011."
"Prepared for the 42nd Plasmadynamics and Lasers Conference sponsored by the American Institute of Aeronautics and Astronautics Honolulu, Hawaii, June 27-30, 2011."
"AIAA-2011-3730."
"This printing replaces NASA/TM--2011-217006, March 2011"--Report documentation page.
Physical Description:1 online resource (31 pages) : color illustrations.
Bibliography:Includes bibliographical references (pages 7-8).