000 | 03187nam a22005535i 4500 | ||
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001 | 978-94-007-6365-4 | ||
003 | DE-He213 | ||
005 | 20140220082942.0 | ||
007 | cr nn 008mamaa | ||
008 | 130426s2013 ne | s |||| 0|eng d | ||
020 |
_a9789400763654 _9978-94-007-6365-4 |
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024 | 7 |
_a10.1007/978-94-007-6365-4 _2doi |
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050 | 4 | _aTA349-359 | |
072 | 7 |
_aTGB _2bicssc |
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072 | 7 |
_aSCI041000 _2bisacsh |
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072 | 7 |
_aTEC009070 _2bisacsh |
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082 | 0 | 4 |
_a620.1 _223 |
100 | 1 |
_aObodan, Natalia I. _eauthor. |
|
245 | 1 | 0 |
_aNonlinear Behaviour and Stability of Thin-Walled Shells _h[electronic resource] / _cby Natalia I. Obodan, Olexandr G. Lebedeyev, Vasilii A. Gromov. |
264 | 1 |
_aDordrecht : _bSpringer Netherlands : _bImprint: Springer, _c2013. |
|
300 |
_aVII, 178 p. 167 illus. _bonline resource. |
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336 |
_atext _btxt _2rdacontent |
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337 |
_acomputer _bc _2rdamedia |
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338 |
_aonline resource _bcr _2rdacarrier |
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347 |
_atext file _bPDF _2rda |
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490 | 1 |
_aSolid Mechanics and Its Applications, _x0925-0042 ; _v199 |
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505 | 0 | _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. | |
520 | _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. | ||
650 | 0 | _aEngineering. | |
650 | 0 |
_aComputer science _xMathematics. |
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650 | 0 | _aEngineering mathematics. | |
650 | 0 | _aMechanical engineering. | |
650 | 0 | _aAstronautics. | |
650 | 1 | 4 | _aEngineering. |
650 | 2 | 4 | _aStructural Mechanics. |
650 | 2 | 4 | _aMechanical Engineering. |
650 | 2 | 4 | _aAppl.Mathematics/Computational Methods of Engineering. |
650 | 2 | 4 | _aAerospace Technology and Astronautics. |
650 | 2 | 4 | _aComputational Mathematics and Numerical Analysis. |
700 | 1 |
_aLebedeyev, Olexandr G. _eauthor. |
|
700 | 1 |
_aGromov, Vasilii A. _eauthor. |
|
710 | 2 | _aSpringerLink (Online service) | |
773 | 0 | _tSpringer eBooks | |
776 | 0 | 8 |
_iPrinted edition: _z9789400763647 |
830 | 0 |
_aSolid Mechanics and Its Applications, _x0925-0042 ; _v199 |
|
856 | 4 | 0 | _uhttp://dx.doi.org/10.1007/978-94-007-6365-4 |
912 | _aZDB-2-ENG | ||
999 |
_c99875 _d99875 |