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035   $a(OCoLC)976012018
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100   $a20170315j199704    ba             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aVertical tail buffeting alleviation using piezoelectric actuators$esome results of the Actively Controlled Response of Buffet-Affected Tails (ACROBAT) program /$fRobert W. Moses
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dApril 1997.
215   $a1 online resource (18 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v110336
300   $a"April 1997."
300   $a"Performing organization: NASA Langley Research Center" Report documentation page.
320   $aIncludes bibliographical references (pages 17-18).
517   $aVertical tail buffeting alleviation using piezoelectric actuators 
606   $aPiezoelectricity$2nasat
606   $aBuffeting$2nasat
606   $aActive control$2nasat
606   $aTail assemblies$2nasat
606   $aSupersonic aircraft$2nasat
606   $aVortices$2nasat
606   $aAngle of attack$2nasat
606   $aAeroelasticity$2nasat
606   $aLeading edges$2nasat
606   $aRoot-mean-square errors$2nasat
615  7$aPiezoelectricity.
615  7$aBuffeting.
615  7$aActive control.
615  7$aTail assemblies.
615  7$aSupersonic aircraft.
615  7$aVortices.
615  7$aAngle of attack.
615  7$aAeroelasticity.
615  7$aLeading edges.
615  7$aRoot-mean-square errors.
700   $aMoses$b Robert W.$01387211
712 02$aLangley Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910708070703321
996   $aVertical tail buffeting alleviation using piezoelectric actuators$93483396
997   $aUNINA