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101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 14$aThe influence of lamination angles on the interior noise levels of an aircraft /$fChristian M. Fernholz, Jay H. Robinson
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dAugust 1996.
215   $a1 online resource (vi, 83 pages)$cillustrations
225 1 $aNASA technical memorandum ;$v110250
300   $aTitle from title screen (viewed June 21, 2016).
300   $a"August 1996."
300   $a"Performing organization: NASA Langley Research Center, Hampton, VA"--Report documentation page.
320   $aIncludes bibliographical references (pages 36-39).
606   $aAircraft production$2nasat
606   $aCylindrical shells$2nasat
606   $aEquations of motion$2nasat
606   $aFinite element method$2nasat
606   $aFrequency ranges$2nasat
606   $aThin walled shells$2nasat
606   $aStructural design criteria$2nasat
606   $aNoise reduction$2nasat
606   $aNoise intensity$2nasat
606   $aLaminates$2nasat
615  7$aAircraft production.
615  7$aCylindrical shells.
615  7$aEquations of motion.
615  7$aFinite element method.
615  7$aFrequency ranges.
615  7$aThin walled shells.
615  7$aStructural design criteria.
615  7$aNoise reduction.
615  7$aNoise intensity.
615  7$aLaminates.
700   $aFernholz$b Christian M$g(Christian Michael),$01402976
702   $aRobinson$b J. H$g(Jay Howard),$f1960-
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910707240203321
996   $aThe influence of lamination angles on the interior noise levels of an aircraft$93474593
997   $aUNINA