{"title":"带三维晶格金字塔型芯的空间四向编织复合材料夹层圆柱壳在谐波载荷和热环境下的频率倍增共振","authors":"Bocheng Dong, Rui Zhao, Kaiping Yu, Jinze Li","doi":"10.1016/j.tws.2025.113260","DOIUrl":null,"url":null,"abstract":"<div><div>In response to the current status of unfulfilled nonlinear dynamics prediction and evaluation tools for novel lightweight spacecraft components, the matched theoretical model and solution procedures for spatial four-direction braided composite sandwich cylindrical shells with three-dimensional lattice pyramid cores are proposed. This will reveal their nonlinear free vibration characteristics and frequency multiplication resonant behaviors. In particular, the nonlinear thermal strains and energy exerted by the thermal expansions are considered by the Green-Lagrange function. The constructed theoretical formulation achieves the equivalent mechanical performance characterization of the three-dimensional lattice pyramid core and spatial four-way braided composites. Based on these explicit expressions, the nonlinear dynamical equations of such a structure subjected to the uniformly distributed harmonic load and thermal environment are derived by employing the first-order shear deformation theory, allowing for the von Kármán geometrical large deformation assumption and the Euler-Lagrange equation. The Green's thermal strain addition terms are introduced. The nonlinear frequencies with initial magnitudes, the amplitude-frequency attributes, and phase trajectories of the primary, super-frequency, and sub-frequency resonances are analytically derived using the multiscale approach. Also, comparison studies are conducted to verify the correctness of the modelling techniques and output data. The manifestations and mechanisms in different nonlinear vibration behaviors are disclosed. Finally, the impact of configuration adjustments and environmental factors on the anti-vibration capability of the structure is characterized via prime dynamic indicators. Some adjustment strategies are reported for pursuing low resonant amplitudes and narrow resonant regions.</div></div>","PeriodicalId":49435,"journal":{"name":"Thin-Walled Structures","volume":"213 ","pages":"Article 113260"},"PeriodicalIF":5.7000,"publicationDate":"2025-03-31","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Frequency multiplication resonances of spatial four-direction braided composite sandwich cylindrical shells with three-dimensional lattice pyramid cores exposed to harmonic loads and thermal environments\",\"authors\":\"Bocheng Dong, Rui Zhao, Kaiping Yu, Jinze Li\",\"doi\":\"10.1016/j.tws.2025.113260\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><div>In response to the current status of unfulfilled nonlinear dynamics prediction and evaluation tools for novel lightweight spacecraft components, the matched theoretical model and solution procedures for spatial four-direction braided composite sandwich cylindrical shells with three-dimensional lattice pyramid cores are proposed. This will reveal their nonlinear free vibration characteristics and frequency multiplication resonant behaviors. In particular, the nonlinear thermal strains and energy exerted by the thermal expansions are considered by the Green-Lagrange function. The constructed theoretical formulation achieves the equivalent mechanical performance characterization of the three-dimensional lattice pyramid core and spatial four-way braided composites. Based on these explicit expressions, the nonlinear dynamical equations of such a structure subjected to the uniformly distributed harmonic load and thermal environment are derived by employing the first-order shear deformation theory, allowing for the von Kármán geometrical large deformation assumption and the Euler-Lagrange equation. The Green's thermal strain addition terms are introduced. The nonlinear frequencies with initial magnitudes, the amplitude-frequency attributes, and phase trajectories of the primary, super-frequency, and sub-frequency resonances are analytically derived using the multiscale approach. Also, comparison studies are conducted to verify the correctness of the modelling techniques and output data. The manifestations and mechanisms in different nonlinear vibration behaviors are disclosed. Finally, the impact of configuration adjustments and environmental factors on the anti-vibration capability of the structure is characterized via prime dynamic indicators. Some adjustment strategies are reported for pursuing low resonant amplitudes and narrow resonant regions.</div></div>\",\"PeriodicalId\":49435,\"journal\":{\"name\":\"Thin-Walled Structures\",\"volume\":\"213 \",\"pages\":\"Article 113260\"},\"PeriodicalIF\":5.7000,\"publicationDate\":\"2025-03-31\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Thin-Walled Structures\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://www.sciencedirect.com/science/article/pii/S0263823125003544\",\"RegionNum\":1,\"RegionCategory\":\"工程技术\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q1\",\"JCRName\":\"ENGINEERING, CIVIL\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Thin-Walled Structures","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S0263823125003544","RegionNum":1,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, CIVIL","Score":null,"Total":0}
Frequency multiplication resonances of spatial four-direction braided composite sandwich cylindrical shells with three-dimensional lattice pyramid cores exposed to harmonic loads and thermal environments
In response to the current status of unfulfilled nonlinear dynamics prediction and evaluation tools for novel lightweight spacecraft components, the matched theoretical model and solution procedures for spatial four-direction braided composite sandwich cylindrical shells with three-dimensional lattice pyramid cores are proposed. This will reveal their nonlinear free vibration characteristics and frequency multiplication resonant behaviors. In particular, the nonlinear thermal strains and energy exerted by the thermal expansions are considered by the Green-Lagrange function. The constructed theoretical formulation achieves the equivalent mechanical performance characterization of the three-dimensional lattice pyramid core and spatial four-way braided composites. Based on these explicit expressions, the nonlinear dynamical equations of such a structure subjected to the uniformly distributed harmonic load and thermal environment are derived by employing the first-order shear deformation theory, allowing for the von Kármán geometrical large deformation assumption and the Euler-Lagrange equation. The Green's thermal strain addition terms are introduced. The nonlinear frequencies with initial magnitudes, the amplitude-frequency attributes, and phase trajectories of the primary, super-frequency, and sub-frequency resonances are analytically derived using the multiscale approach. Also, comparison studies are conducted to verify the correctness of the modelling techniques and output data. The manifestations and mechanisms in different nonlinear vibration behaviors are disclosed. Finally, the impact of configuration adjustments and environmental factors on the anti-vibration capability of the structure is characterized via prime dynamic indicators. Some adjustment strategies are reported for pursuing low resonant amplitudes and narrow resonant regions.
期刊介绍:
Thin-walled structures comprises an important and growing proportion of engineering construction with areas of application becoming increasingly diverse, ranging from aircraft, bridges, ships and oil rigs to storage vessels, industrial buildings and warehouses.
Many factors, including cost and weight economy, new materials and processes and the growth of powerful methods of analysis have contributed to this growth, and led to the need for a journal which concentrates specifically on structures in which problems arise due to the thinness of the walls. This field includes cold– formed sections, plate and shell structures, reinforced plastics structures and aluminium structures, and is of importance in many branches of engineering.
The primary criterion for consideration of papers in Thin–Walled Structures is that they must be concerned with thin–walled structures or the basic problems inherent in thin–walled structures. Provided this criterion is satisfied no restriction is placed on the type of construction, material or field of application. Papers on theory, experiment, design, etc., are published and it is expected that many papers will contain aspects of all three.