Design of rectangular sandwich panels with metal skins based on post-buckling state in compression and shear
Solutions of geometrically non-linear tasks concerning post-buckling behavior of sandwich panels with thin metal skins and lightweight filler loaded by compression and shear flows are shown. Based on obtained solutions methods of aircraft structures sandwich panels design based on post-buckling stat...
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| Veröffentlicht in: | IOP conference series. Materials Science and Engineering 2019-11, Vol.684 (1), p.12020 |
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| creator | Mitrofanov, O V |
| description | Solutions of geometrically non-linear tasks concerning post-buckling behavior of sandwich panels with thin metal skins and lightweight filler loaded by compression and shear flows are shown. Based on obtained solutions methods of aircraft structures sandwich panels design based on post-buckling state with acceptable global buckling in case of ultimate loading are suggested. |
| doi_str_mv | 10.1088/1757-899X/684/1/012020 |
| format | Article |
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| ispartof | IOP conference series. Materials Science and Engineering, 2019-11, Vol.684 (1), p.12020 |
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| language | eng |
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| source | IOP Publishing Free Content; Elektronische Zeitschriftenbibliothek - Frei zugängliche E-Journals; IOPscience extra; Free Full-Text Journals in Chemistry |
| subjects | Aircraft design Aircraft structures Postbuckling Sandwich panels Shear flow |
| title | Design of rectangular sandwich panels with metal skins based on post-buckling state in compression and shear |
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