Coupled higher-order layerwise mechanics and finite element formulations for laminated composite beams with active SMA layers
Identifikátory výsledku
Kód výsledku v IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68378271%3A_____%2F24%3A00588246" target="_blank" >RIV/68378271:_____/24:00588246 - isvavai.cz</a>
Výsledek na webu
<a href="https://doi.org/10.1016/j.euromechsol.2024.105380" target="_blank" >https://doi.org/10.1016/j.euromechsol.2024.105380</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1016/j.euromechsol.2024.105380" target="_blank" >10.1016/j.euromechsol.2024.105380</a>
Alternativní jazyky
Jazyk výsledku
angličtina
Název v původním jazyce
Coupled higher-order layerwise mechanics and finite element formulations for laminated composite beams with active SMA layers
Popis výsledku v původním jazyce
This study proposes a thermo-elastic coupled nonlinear finite element (FE) model for laminated composite beams with active SMA layers based on a higher-order layerwise theory and Brinson's model of SMA's phase transformation constitutive relations. The developed FE Model is further discretized by using the Newton-Raphson time integration scheme to update SMA's phase transformation progress step by step. This new model can be used for thermal-mechanical behavior analysis of hybrid SMA-composite laminated beams, which especially enables accurate prediction for static response of moderately thick to thick beams, large deformation analysis, through-thickness variations of interlaminar stresses and strains. The accuracy and effectiveness of the proposed approach are verified by several numerical examples, and the results are compared with those obtained from corresponding alternative solutions and experimental tests. Using the developed FEM, the effects of temperature, geometrical nonlinearity, pre-strain of SMA, and stacking sequence of composite laminates on the static response of hybrid SMA-composite beams are studied.n
Název v anglickém jazyce
Coupled higher-order layerwise mechanics and finite element formulations for laminated composite beams with active SMA layers
Popis výsledku anglicky
This study proposes a thermo-elastic coupled nonlinear finite element (FE) model for laminated composite beams with active SMA layers based on a higher-order layerwise theory and Brinson's model of SMA's phase transformation constitutive relations. The developed FE Model is further discretized by using the Newton-Raphson time integration scheme to update SMA's phase transformation progress step by step. This new model can be used for thermal-mechanical behavior analysis of hybrid SMA-composite laminated beams, which especially enables accurate prediction for static response of moderately thick to thick beams, large deformation analysis, through-thickness variations of interlaminar stresses and strains. The accuracy and effectiveness of the proposed approach are verified by several numerical examples, and the results are compared with those obtained from corresponding alternative solutions and experimental tests. Using the developed FEM, the effects of temperature, geometrical nonlinearity, pre-strain of SMA, and stacking sequence of composite laminates on the static response of hybrid SMA-composite beams are studied.n
Klasifikace
Druh
J<sub>imp</sub> - Článek v periodiku v databázi Web of Science
CEP obor
—
OECD FORD obor
10302 - Condensed matter physics (including formerly solid state physics, supercond.)
Návaznosti výsledku
Projekt
—
Návaznosti
I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace
Ostatní
Rok uplatnění
2024
Kód důvěrnosti údajů
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Údaje specifické pro druh výsledku
Název periodika
European Journal of Mechanics A-Solids
ISSN
0997-7538
e-ISSN
1873-7285
Svazek periodika
107
Číslo periodika v rámci svazku
Sep-Oct
Stát vydavatele periodika
NL - Nizozemsko
Počet stran výsledku
13
Strana od-do
105380
Kód UT WoS článku
001266253200001
EID výsledku v databázi Scopus
2-s2.0-85197287935