LEADER 01569nam a2200481 i 4500 001 991000954989707536 005 20020507180533.0 008 930628s1991 ||| ||| | eng 020 $a3540547282 035 $ab10780816-39ule_inst 035 $aLE01304838$9ExL 040 $aDip.to Matematica$beng 082 0 $a516.36 084 $aAMS 53-06 084 $aAMS 53A04 084 $aAMS 53A07 084 $aAMS 53A10 084 $aAMS 53A15 084 $aAMS 53A60 084 $aAMS 53C30 084 $aAMS 53C42 084 $aAMS 58-06 084 $aAMS 58A50 084 $aAMS 58D05 084 $aAMS 58E05 084 $aAMS 58G25 084 $aAMS 58G30 100 1 $aFerus, Dirk$056777 245 10$aGlobal differential geometry and global analysis :$bproc. of a conference held in Berlin, 15-20 June, 1990 /$ceds. D. Ferus, U. Pinkall, U. Simon, B. Wegner 260 $aBerlin :$bSpringer-Verlag,$c1991 300 $aviii, 282 p. ;$c24 cm 490 0 $aLecture notes in mathematics,$x0075-8434 ;$v1481 650 4$aDifferential geometry$xCongresses 650 4$aGlobal analysis$xCongresses 700 1 $aPinkall, Ulrich 700 1 $aSimon, Udo 700 1 $aWegner, Bernd 907 $a.b10780816$b23-02-17$c28-06-02 912 $a991000954989707536 945 $aLE013 53-XX FER13 (1991)$g1$i2013000033334$lle013$o-$pE0.00$q-$rl$s- $t0$u1$v0$w1$x0$y.i10880458$z28-06-02 996 $aGlobal differential geometry and global analysis$9383676 997 $aUNISALENTO 998 $ale013$b01-01-93$cm$da $e-$feng$gxx $h0$i1 LEADER 02106nam 2200577I 450 001 9910702094303321 005 20130131132409.0 035 $a(CKB)5470000002423181 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