02106nam 2200577I 450 991070209430332120130131132409.0(CKB)5470000002423181(OCoLC)826166163(EXLCZ)99547000000242318120130131d2012 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierThe exact solution for linear thermoelastic axisymmetric deformations of generally laminated circular cylindrical shells /Michael P. Nemeth and Marc R. SchultzHampton, Va. :National Aeronautics and Space Administration, Langley Research Center,[2012]1 online resource (99 pages) color illustrations[NASA technical paper] ;NASA/TP 2012-217342Title from title screen (viewed Jan. 31, 2013)."February 2012."Includes bibliographical references (pages 50-52).AnisotropynasatCylindrical shellsnasatBoundary conditionsnasatComposite structuresnasatSurface temperaturenasatTemperature distributionnasatThermoelasticitynasatLaminatesnasatAxial strainnasatAnisotropy.Cylindrical shells.Boundary conditions.Composite structures.Surface temperature.Temperature distribution.Thermoelasticity.Laminates.Axial strain.Nemeth Michael P.1391721Schultz Marc R.Langley Research Center,United States.National Aeronautics and Space Administration,GPOGPOBOOK9910702094303321The exact solution for linear thermoelastic axisymmetric deformations of generally laminated circular cylindrical shells3529100UNINA