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

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

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https://purl.fdlp.gov/GPO/gpo45706

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Call Number: NAS 1.15:2011-217006/REV.1
 
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