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100   $a20110914d2006      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aFinite and boundary element modeling of the NASA Langley aluminum testbed cylinder (ATC)$b[electronic resource] /$fFerdinand W. Grosveld
210  1$aHampton, Va. :$cNational Aeronautics and Space Administration, Langley Research Center,$d[2006]
215   $a1 online resource (72 pages) $ccolor illustrations
225 1 $aNASA/CR ;$v2006-214283
300   $aTitle from title screen (viewed on Sept. 14, 2011).
300   $a"March 2006."
320   $aIncludes bibliographical references (pages 19-20).
410  0$aNASA contractor report ;$vNASA CR-214283.
517   $aFinite and boundary element modeling of the NASA Langley aluminum testbed cylinder 
606   $aAcoustics$2nasat
606   $aAluminum$2nasat
606   $aFinite element method$2nasat
606   $aMathematical models$2nasat
606   $aCircular cylinders$2nasat
615  7$aAcoustics.
615  7$aAluminum.
615  7$aFinite element method.
615  7$aMathematical models.
615  7$aCircular cylinders.
700   $aGrosveld$b Ferdinand W$01391334
712 02$aLangley Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910697289703321
996   $aFinite and boundary element modeling of the NASA Langley aluminum testbed cylinder (ATC)$93445055
997   $aUNINA