02216nam 2200601I 450 991070211040332120130115150815.0(CKB)5470000002425038(OCoLC)824456172(EXLCZ)99547000000242503820130115d2012 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierShock generation and control using DBD plasma actuators SBIR phase I final report /by Mehul P. Patel [and four others]Cleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,[2012]1 online resource (34 pages) color illustrations[NASA contractor report] ;NASA-CR 2012-217448Title from title screen (viewed Jan. 15, 2013)."June 2012.""This work was sponsored by the Fundamental Aeronautics Program at the NASA Glenn Research Center."Includes bibliographical references (pages 33-34).Shock generation and control using DBD plasma actuators ActuatorsnasatDielectricsnasatShock testsnasatWind tunnel testsnasatAircraft enginesnasatTurbulent boundary layernasatBoundary layer separationnasatSupersonic inletsnasatOblique shock wavesnasatActuators.Dielectrics.Shock tests.Wind tunnel tests.Aircraft engines.Turbulent boundary layer.Boundary layer separation.Supersonic inlets.Oblique shock waves.Patel Mehul P.1387839NASA Glenn Research Center,Fundamental Aeronautics Program (U.S.),United States.National Aeronautics and Space Administration,GPOGPOBOOK9910702110403321Shock generation and control using DBD plasma actuators3438048UNINA