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035   $a(OCoLC)826166163
035   $a(EXLCZ)995470000002423181
100   $a20130131d2012      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 14$aThe exact solution for linear thermoelastic axisymmetric deformations of generally laminated circular cylindrical shells /$fMichael P. Nemeth and Marc R. Schultz
210  1$aHampton, Va. :$cNational Aeronautics and Space Administration, Langley Research Center,$d[2012]
215   $a1 online resource (99 pages) $ccolor illustrations
225 1 $a[NASA technical paper] ;$vNASA/TP 2012-217342
300   $aTitle from title screen (viewed Jan. 31, 2013).
300   $a"February 2012."
320   $aIncludes bibliographical references (pages 50-52).
606   $aAnisotropy$2nasat
606   $aCylindrical shells$2nasat
606   $aBoundary conditions$2nasat
606   $aComposite structures$2nasat
606   $aSurface temperature$2nasat
606   $aTemperature distribution$2nasat
606   $aThermoelasticity$2nasat
606   $aLaminates$2nasat
606   $aAxial strain$2nasat
615  7$aAnisotropy.
615  7$aCylindrical shells.
615  7$aBoundary conditions.
615  7$aComposite structures.
615  7$aSurface temperature.
615  7$aTemperature distribution.
615  7$aThermoelasticity.
615  7$aLaminates.
615  7$aAxial strain.
700   $aNemeth$b Michael P.$01391721
702   $aSchultz$b Marc R.
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702094303321
996   $aThe exact solution for linear thermoelastic axisymmetric deformations of generally laminated circular cylindrical shells$93529100
997   $aUNINA