Eine Plattform für die Wissenschaft: Bauingenieurwesen, Architektur und Urbanistik
Eine Plattform für die Wissenschaft: Bauingenieurwesen, Architektur und Urbanistik
Nonlinear vibration of the sandwich beam with auxetic honeycomb core under thermal shock
https://orcid.org/0000-0001-6396-6054
Highlights Effects of heating and cooling thermal shock on thermally induced vibration (TIV) are explored. Influence of geometric nonlinearity under heating/cooling thermal shock forms is revealed. The TIV characteristics of sandwich beams with auxetic honeycomb cores are discussed and compared with traditional honeycomb. The instability conditions of the clamped beam with immovable ends under heating thermal shock are given.
Abstract The nonlinear thermally induced vibration (TIV) characteristics of sandwich beams with auxetic honeycomb cores under general boundary conditions are studied. Based on first-order shear deformation theory, the dynamic governing equations are obtained through Hamilton principle, in which geometric nonlinearity and temperature dependence are considered. The temperature field along the thickness is calculated by finite element method and nonlinear TIV responses are solved via Newton-Raphson-Newmark method. The effects of temperature dependency, thermal shock forms, geometric nonlinearity, thicknesses of beam and face-sheet, boundaries and honeycomb geometrical parameters are studied. Results show that the reduction of the absolute inclined angle of the auxetic honeycomb can weaken the TIV responses. The influence of geometric nonlinearity on quasi-static and dynamic responses depends on the thermal shock form. Thermal buckling is the necessary condition for the occurrence of the TIV in clamped beams with immovable ends. Moreover, the research provides some design references to suppress the TIV responses of the sandwich beam with auxetic honeycomb core.
Nonlinear vibration of the sandwich beam with auxetic honeycomb core under thermal shock
https://orcid.org/0000-0001-6396-6054
Highlights Effects of heating and cooling thermal shock on thermally induced vibration (TIV) are explored. Influence of geometric nonlinearity under heating/cooling thermal shock forms is revealed. The TIV characteristics of sandwich beams with auxetic honeycomb cores are discussed and compared with traditional honeycomb. The instability conditions of the clamped beam with immovable ends under heating thermal shock are given.
Abstract The nonlinear thermally induced vibration (TIV) characteristics of sandwich beams with auxetic honeycomb cores under general boundary conditions are studied. Based on first-order shear deformation theory, the dynamic governing equations are obtained through Hamilton principle, in which geometric nonlinearity and temperature dependence are considered. The temperature field along the thickness is calculated by finite element method and nonlinear TIV responses are solved via Newton-Raphson-Newmark method. The effects of temperature dependency, thermal shock forms, geometric nonlinearity, thicknesses of beam and face-sheet, boundaries and honeycomb geometrical parameters are studied. Results show that the reduction of the absolute inclined angle of the auxetic honeycomb can weaken the TIV responses. The influence of geometric nonlinearity on quasi-static and dynamic responses depends on the thermal shock form. Thermal buckling is the necessary condition for the occurrence of the TIV in clamped beams with immovable ends. Moreover, the research provides some design references to suppress the TIV responses of the sandwich beam with auxetic honeycomb core.
Nonlinear vibration of the sandwich beam with auxetic honeycomb core under thermal shock
https://orcid.org/0000-0001-6396-6054
Highlights Effects of heating and cooling thermal shock on thermally induced vibration (TIV) are explored. Influence of geometric nonlinearity under heating/cooling thermal shock forms is revealed. The TIV characteristics of sandwich beams with auxetic honeycomb cores are discussed and compared with traditional honeycomb. The instability conditions of the clamped beam with immovable ends under heating thermal shock are given.
Abstract The nonlinear thermally induced vibration (TIV) characteristics of sandwich beams with auxetic honeycomb cores under general boundary conditions are studied. Based on first-order shear deformation theory, the dynamic governing equations are obtained through Hamilton principle, in which geometric nonlinearity and temperature dependence are considered. The temperature field along the thickness is calculated by finite element method and nonlinear TIV responses are solved via Newton-Raphson-Newmark method. The effects of temperature dependency, thermal shock forms, geometric nonlinearity, thicknesses of beam and face-sheet, boundaries and honeycomb geometrical parameters are studied. Results show that the reduction of the absolute inclined angle of the auxetic honeycomb can weaken the TIV responses. The influence of geometric nonlinearity on quasi-static and dynamic responses depends on the thermal shock form. Thermal buckling is the necessary condition for the occurrence of the TIV in clamped beams with immovable ends. Moreover, the research provides some design references to suppress the TIV responses of the sandwich beam with auxetic honeycomb core.
Nonlinear vibration of the sandwich beam with auxetic honeycomb core under thermal shock
Li, P.Q. (Autor:in) / Wang, K.F. (Autor:in) / Wang, B.L. (Autor:in)
Thin-Walled Structures ; 196
09.12.2023
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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