LEADER 02216nam  2200601I  450 
001 9910702110403321
005 20130115150815.0
035   $a(CKB)5470000002425038
035   $a(OCoLC)824456172
035   $a(EXLCZ)995470000002425038
100   $a20130115d2012      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aShock generation and control using DBD plasma actuators $eSBIR phase I final report /$fby Mehul P. Patel [and four others]
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2012]
215   $a1 online resource (34 pages) $ccolor illustrations
225 1 $a[NASA contractor report] ;$vNASA-CR 2012-217448
300   $aTitle from title screen (viewed Jan. 15, 2013).
300   $a"June 2012."
300   $a"This work was sponsored by the Fundamental Aeronautics Program at the NASA Glenn Research Center."
320   $aIncludes bibliographical references (pages 33-34).
517   $aShock generation and control using DBD plasma actuators 
606   $aActuators$2nasat
606   $aDielectrics$2nasat
606   $aShock tests$2nasat
606   $aWind tunnel tests$2nasat
606   $aAircraft engines$2nasat
606   $aTurbulent boundary layer$2nasat
606   $aBoundary layer separation$2nasat
606   $aSupersonic inlets$2nasat
606   $aOblique shock waves$2nasat
615  7$aActuators.
615  7$aDielectrics.
615  7$aShock tests.
615  7$aWind tunnel tests.
615  7$aAircraft engines.
615  7$aTurbulent boundary layer.
615  7$aBoundary layer separation.
615  7$aSupersonic inlets.
615  7$aOblique shock waves.
700   $aPatel$b Mehul P.$01387839
712 02$aNASA Glenn Research Center,
712 02$aFundamental Aeronautics Program (U.S.),
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702110403321
996   $aShock generation and control using DBD plasma actuators$93438048
997   $aUNINA