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001 9910704382203321
005 20170816115022.0
035   $a(CKB)5470000002439860
035   $a(OCoLC)755236736
035   $a(EXLCZ)995470000002439860
100   $a20110930j199711    ua             0
101 0 $aeng
135   $aurbn||||a|a||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 12$aA feasibility study to control airfoil shape using THUNDER /$fJennifer L. Pinkerton and Robert W. Moses
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dNovember 1997.
215   $a1 online resource (26 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v4767
300   $aTitle from title screen (viewed March 2, 2016).
300   $a"November 1997."
300   $a"Performing organization: NASA Langley Research Center, Hampton, VA"--Report documentation page.
320   $aIncludes bibliographical references (pages 8-9).
517 3 $aFeasibility study to control airfoil shape using thin-layer composite-unimorph ferroelectric driver and sensor
606   $aActuators$2nasat
606   $aHysteresis$2nasat
606   $aAirfoil profiles$2nasat
606   $aPiezoelectricity$2nasat
606   $aFerroelectricity$2nasat
615  7$aActuators.
615  7$aHysteresis.
615  7$aAirfoil profiles.
615  7$aPiezoelectricity.
615  7$aFerroelectricity.
700   $aPinkerton$b Jennifer L.$01408709
702   $aMoses$b Robert W.
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCO
801  2$bGPO
906   $aBOOK
912   $a9910704382203321
996   $aA feasibility study to control airfoil shape using THUNDER$93493247
997   $aUNINA