LEADER 03141nam 2200625Ia 450 001 9910438052503321 005 20200520144314.0 010 $a94-007-6365-4 024 7 $a10.1007/978-94-007-6365-4 035 $a(CKB)2670000000372377 035 $a(EBL)1697552 035 $a(OCoLC)842123188 035 $a(SSID)ssj0000908086 035 $a(PQKBManifestationID)11470729 035 $a(PQKBTitleCode)TC0000908086 035 $a(PQKBWorkID)10897997 035 $a(PQKB)11484561 035 $a(DE-He213)978-94-007-6365-4 035 $a(MiAaPQ)EBC1697552 035 $a(PPN)16914254X 035 $a(EXLCZ)992670000000372377 100 $a20111102d2013 uy 0 101 0 $aeng 135 $aur|n|---||||| 181 $ctxt 182 $cc 183 $acr 200 10$aNonlinear behavior and stability of thin-walled shells /$fNatalia I. Obodan, Olexandr G. Lebedeyev, Vasilii A. Gromov 205 $a1st ed. 2013. 210 $aDordrecht $cSpringer$dc2013 215 $a1 online resource (182 p.) 225 1 $aSolid Mechanics and Its Applications,$x0925-0042 ;$v199 300 $aDescription based upon print version of record. 311 $a94-017-8489-2 311 $a94-007-6364-6 320 $aIncludes bibliographical references. 327 $a1. In lieu of introduction -- 2. Boundary problem of thin shells theory -- 3. Branching of nonlinear boundary problem solutions -- 4. Numerical method -- 5. Nonaxisymmetrically loaded cylindrical shell -- 6. Structurally nonaxisymetric shell subjected to uniform loading -- 7. Postcritical branching patterns for cylindrical shell subjected to uniform external loading -- 8. Postbuckling behaviour and stability of anisotropic shells -- 9. Conclusion. 330 $aThis book focuses on the nonlinear behaviour of thin-wall shells (single- and multilayered with delamination areas) under various uniform and non-uniform loadings. The dependence of critical (buckling) load upon load variability is revealed to be highly non-monotonous, showing minima when load variability is close to the eigenmode variabilities of solution branching points of the respective nonlinear boundary problem. A novel numerical approach is employed to analyze branching points and to build primary, secondary, and tertiary bifurcation paths of the nonlinear boundary problem for the case of uniform loading. The load levels of singular points belonging to the paths are considered to be critical load estimates for the case of non-uniform loadings. 410 0$aSolid Mechanics and Its Applications,$x0925-0042 ;$v199 606 $aThin-walled structures 606 $aShells (Engineering) 615 0$aThin-walled structures. 615 0$aShells (Engineering) 676 $a515.355 676 $a515/.355 700 $aObodan$b Natalia I$01060453 701 $aLebedeyev$b Olexandr G$01762477 701 $aGromov$b Vasilii A. $01762478 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910438052503321 996 $aNonlinear behavior and stability of thin-walled shells$94202463 997 $aUNINA