LEADER 01964nam  2200529I  450 
001 9910702354503321
005 20140812161536.0
035   $a(CKB)5470000002426613
035   $a(OCoLC)886551433
035   $a(EXLCZ)995470000002426613
100   $a20140812d2012      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aPiezoelectric vibration damping study for rotating composite fan blades /$fJames B. Min [and four others]
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d2012.
215   $a1 online resource (25 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2012-217648
300   $aTitle from title screen (viewed on Aug. 12, 2014).
300   $a"August 2012."
300   $a"Prepared for the 53rd Structures, Structural Dynamics, and Materials Conference cosponsored by the AIAA, ASME, ASCE, AHS, and ASC, Honolulu, Hawaii, April 23-26, 2012."
320   $aIncludes bibliographical references (pages 24-25).
606   $aPiezoelectricity$2nasat
606   $aFan blades$2nasat
606   $aHarmonic analysis$2nasat
606   $aResonant vibration$2nasat
606   $aVibration damping$2nasat
606   $aMathematical models$2nasat
606   $aFinite element method$2nasat
615  7$aPiezoelectricity.
615  7$aFan blades.
615  7$aHarmonic analysis.
615  7$aResonant vibration.
615  7$aVibration damping.
615  7$aMathematical models.
615  7$aFinite element method.
700   $aMin$b James B.$01407296
712 02$aNASA Glenn Research Center,
712 02$aFundamental Aeronautics Program (U.S.),
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702354503321
996   $aPiezoelectric vibration damping study for rotating composite fan blades$93511072
997   $aUNINA