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035   $a(CKB)5470000002423730
035   $a(OCoLC)809195079
035   $a(EXLCZ)995470000002423730
100   $a20120905d2004      ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aDevelopment of an actuator for flow control utilizing detonation$b[electronic resource] /$fPatrick J. Lonneman and Andrew D. Cutler
210  1$aHampton, Va. :$cNational Aeronautics and Space Administration, Langley Research Center,$d[2004]
215   $a1 online resource (xvi, 156 pages) $cillustrations (some color)
225 1 $aNASA/CR ;$v2004-213508
300   $aTitle from title screen (viewed on Sept. 5, 2012).
300   $a"December 2004."
300   $a"Performing organization, The George Washington University, Joint Institute for Advancement of Flight Sciences, Langley Research Center"--Rept. documentation p.
320   $aIncludes bibliographical references (pages 56-58).
606   $aActive control$2nasat
606   $aFlow distribution$2nasat
606   $aSeparated flow$2nasat
606   $aDetonation$2nasat
606   $aActuators$2nasat
606   $aFlow regulators$2nasat
615  7$aActive control.
615  7$aFlow distribution.
615  7$aSeparated flow.
615  7$aDetonation.
615  7$aActuators.
615  7$aFlow regulators.
700   $aLonneman$b Patrick J$01416133
701   $aCutler$b Andrew D$01416134
712 02$aJoint Institute for Advancement of Flight Sciences.
712 02$aLangley Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702039903321
996   $aDevelopment of an actuator for flow control utilizing detonation$93520386
997   $aUNINA