LEADER 01853nam  2200493Ia 450 
001 9910701118603321
005 20111221105130.0
035   $a(CKB)5470000002415865
035   $a(OCoLC)768998234
035   $a(EXLCZ)995470000002415865
100   $a20111221d2011      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aStatistical Energy Analysis (SEA) and Energy Finite Element Analysis (EFEA) predictions for a floor-equipped composite cylinder$b[electronic resource] /$fFerdinand W. Grosveld, Noah H. Schiller and Randolph H. Cabell
210  1$aHampton, Va. :$cNational Aeronautics and Space Administration, Langley Research Center,$d[2011]
215   $a1 online resource (44 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2011-217171
300   $aTitle from title screen (viewed on Dec. 21, 2011).
300   $a"August 2011."
320   $aIncludes bibliographical references (pages 17-18).
517   $aStatistical Energy Analysis 
606   $aComets$2nasat
606   $aFinite element method$2nasat
606   $aVibrational stress$2nasat
606   $aAcoustics$2nasat
606   $aStatistical analysis$2nasat
615  7$aComets.
615  7$aFinite element method.
615  7$aVibrational stress.
615  7$aAcoustics.
615  7$aStatistical analysis.
700   $aGrosveld$b Ferdinand W$01391334
701   $aSchiller$b Noah H$01392070
701   $aCabell$b Randolph H$055389
712 02$aLangley Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910701118603321
996   $aStatistical Energy Analysis (SEA) and Energy Finite Element Analysis (EFEA) predictions for a floor-equipped composite cylinder$93446365
997   $aUNINA