DBD plasma actuators for flow control in air vehicles and jet engines : simulation of flight conditions in test chambers by density matching / David E. Ashpis, Douglas R. Thurman.

Author/creator Ashpis, D. E. author.
Format Electronic
Edition[Revised].
PublicationCleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2011.
Description1 online resource (31 pages) : color illustrations.
Supplemental Contenthttps://purl.fdlp.gov/GPO/gpo45706

Other author/creatorThurman, Douglas R., author.
Other author/creatorNASA Glenn Research Center, issuing body.
Other author/creatorUnited States. National Aeronautics and Space Administration sponsoring body.
Other author/creatorU.S. Army Research Laboratory, sponsoring body.
Uniform titleDBD plasma actuators for flow control in air vehicles and jet engines (Revised July 2011)
Variant title Dielectric Barrier Discharge plasma actuators for flow control in air vehicles and jet engines
SeriesNASA/TM ; 2011-217006/REV1
NASA technical memorandum 2011-217006/REV 1. ^A467613
General noteTitle from title screen (viewed on Feb. 4, 2014).
General note"July 2011."
General note"Prepared for the 42nd Plasmadynamics and Lasers Conference sponsored by the American Institute of Aeronautics and Astronautics Honolulu, Hawaii, June 27-30, 2011."
General note"AIAA-2011-3730."
General note"This printing replaces NASA/TM--2011-217006, March 2011"--Report documentation page.
General noteGPO Cataloging Record Distribution Program (CRDP).
Bibliography noteIncludes bibliographical references (pages 7-8).
Funding informationSponsored by National Aeronautics and Space Administration and U.S. Army Research Laboratory WBS 561581.02.08.03.21.13.02
Funding informationE-17602-1
GPO item number0830-D (online)
Govt. docs number NAS 1.15:2011-217006/REV.1