LEADER 02106nam  2200577   450 
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035   $a(CKB)5470000002427633
035   $a(OCoLC)825823048
035   $a(EXLCZ)995470000002427633
100   $a20130129d2012      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aPlasma actuators for turbomachinery flow control, final report /$fRichard B. Miles and Mikhail N. Shneider
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2012]
215   $a1 online resource (55 pages) $ccolor illustrations
225 1 $a[NASA contractor report] ;$vNASA-CR 2012-217654
300   $aTitle from title screen (viewed Jan. 29, 2013).
300   $a"September 2012."
300   $a"This work was sponsored by the Fundamental Aeronautics Program at the NASA Glenn Research Center."
320   $aIncludes bibliographical references.
606   $aTurbomachinery$2nasat
606   $aDielectrics$2nasat
606   $aMagnetohydrodynamic flow$2nasat
606   $aThrust reversal$2nasat
606   $aSemiconductor diodes$2nasat
606   $aElectrical faults$2nasat
606   $aActuators$2nasat
606   $aElectric potential$2nasat
615  7$aTurbomachinery.
615  7$aDielectrics.
615  7$aMagnetohydrodynamic flow.
615  7$aThrust reversal.
615  7$aSemiconductor diodes.
615  7$aElectrical faults.
615  7$aActuators.
615  7$aElectric potential.
700   $aMiles$b Richard B$g(Richard Bryant),$f1948-$01396727
702   $aShneider$b Mikhail N.
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   $a9910702453503321
996   $aPlasma actuators for turbomachinery flow control, final report$93457237
997   $aUNINA