{"title":"一种集稳定力学性能、两个平台应力阶段和泊松比符号转换为一体的新型多功能多弧增强圆柱形元结构","authors":"Hao Xu, Hai-Tao Liu","doi":"10.1016/j.ast.2025.110958","DOIUrl":null,"url":null,"abstract":"<div><div>The increase in energy absorption is often accompanied by an increase in stiffness, which will exacerbate structural damage under compressive load. Based on multi-arc enhanced re-entrant honeycomb, a novel multi-arc enhanced cylindrical metastructure (MAECM) is designed in this paper to solve the conflict between stiffness and energy absorption. The new metastructure exhibits two plateau stress stages, Poisson's ratio sign-switching, and constant Poisson's ratio. Specimens with different parameters are printed, and the corresponding finite element models are established. The effects of various parameters on mechanical properties are investigated by finite element analysis and experiment. Results show that the two plateau stress stages and Poisson's ratio sign-switching can be achieved through the self-contact of the connecting rods. The constant Poisson's ratio can be achieved under specific geometric parameters to achieve stable mechanical properties of the structure. The geometric parameters can effectively adjust the Young's modulus, specific energy absorption (SEA), Poisson's ratio, contact strain, and sign-switching strain of the structure. Compared with the original structure, the Young's modulus of MAECM has decreased by 67 %, and the energy absorption has increased by 164 %. The various mechanical properties, low stiffness, and superior energy absorption capacity of MAECM make it more advantageous than other proposed structures. These outstanding mechanical properties enable MAECM to solve the conflict between stiffness and energy absorption. The lower Young's modulus and adjustable Poisson's ratio enable MAECM to be used as the internal supporting substructure of the missile skin. The deformation of the MAECM can achieve the adjustment of the missile's motion attitude. MAECM expands the application of metastructures in the aerospace field and provides a novel method for designing multifunctional metastructures.</div></div>","PeriodicalId":50955,"journal":{"name":"Aerospace Science and Technology","volume":"168 ","pages":"Article 110958"},"PeriodicalIF":5.8000,"publicationDate":"2025-09-17","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"A new multifunctional multi-arc enhanced cylindrical metastructure integrating stable mechanical properties, two plateau stress stages, and Poisson's ratio sign-switching\",\"authors\":\"Hao Xu, Hai-Tao Liu\",\"doi\":\"10.1016/j.ast.2025.110958\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><div>The increase in energy absorption is often accompanied by an increase in stiffness, which will exacerbate structural damage under compressive load. Based on multi-arc enhanced re-entrant honeycomb, a novel multi-arc enhanced cylindrical metastructure (MAECM) is designed in this paper to solve the conflict between stiffness and energy absorption. The new metastructure exhibits two plateau stress stages, Poisson's ratio sign-switching, and constant Poisson's ratio. Specimens with different parameters are printed, and the corresponding finite element models are established. The effects of various parameters on mechanical properties are investigated by finite element analysis and experiment. Results show that the two plateau stress stages and Poisson's ratio sign-switching can be achieved through the self-contact of the connecting rods. The constant Poisson's ratio can be achieved under specific geometric parameters to achieve stable mechanical properties of the structure. The geometric parameters can effectively adjust the Young's modulus, specific energy absorption (SEA), Poisson's ratio, contact strain, and sign-switching strain of the structure. Compared with the original structure, the Young's modulus of MAECM has decreased by 67 %, and the energy absorption has increased by 164 %. The various mechanical properties, low stiffness, and superior energy absorption capacity of MAECM make it more advantageous than other proposed structures. These outstanding mechanical properties enable MAECM to solve the conflict between stiffness and energy absorption. The lower Young's modulus and adjustable Poisson's ratio enable MAECM to be used as the internal supporting substructure of the missile skin. The deformation of the MAECM can achieve the adjustment of the missile's motion attitude. MAECM expands the application of metastructures in the aerospace field and provides a novel method for designing multifunctional metastructures.</div></div>\",\"PeriodicalId\":50955,\"journal\":{\"name\":\"Aerospace Science and Technology\",\"volume\":\"168 \",\"pages\":\"Article 110958\"},\"PeriodicalIF\":5.8000,\"publicationDate\":\"2025-09-17\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Aerospace Science and Technology\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://www.sciencedirect.com/science/article/pii/S1270963825010181\",\"RegionNum\":1,\"RegionCategory\":\"工程技术\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q1\",\"JCRName\":\"ENGINEERING, AEROSPACE\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Aerospace Science and Technology","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S1270963825010181","RegionNum":1,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
A new multifunctional multi-arc enhanced cylindrical metastructure integrating stable mechanical properties, two plateau stress stages, and Poisson's ratio sign-switching
The increase in energy absorption is often accompanied by an increase in stiffness, which will exacerbate structural damage under compressive load. Based on multi-arc enhanced re-entrant honeycomb, a novel multi-arc enhanced cylindrical metastructure (MAECM) is designed in this paper to solve the conflict between stiffness and energy absorption. The new metastructure exhibits two plateau stress stages, Poisson's ratio sign-switching, and constant Poisson's ratio. Specimens with different parameters are printed, and the corresponding finite element models are established. The effects of various parameters on mechanical properties are investigated by finite element analysis and experiment. Results show that the two plateau stress stages and Poisson's ratio sign-switching can be achieved through the self-contact of the connecting rods. The constant Poisson's ratio can be achieved under specific geometric parameters to achieve stable mechanical properties of the structure. The geometric parameters can effectively adjust the Young's modulus, specific energy absorption (SEA), Poisson's ratio, contact strain, and sign-switching strain of the structure. Compared with the original structure, the Young's modulus of MAECM has decreased by 67 %, and the energy absorption has increased by 164 %. The various mechanical properties, low stiffness, and superior energy absorption capacity of MAECM make it more advantageous than other proposed structures. These outstanding mechanical properties enable MAECM to solve the conflict between stiffness and energy absorption. The lower Young's modulus and adjustable Poisson's ratio enable MAECM to be used as the internal supporting substructure of the missile skin. The deformation of the MAECM can achieve the adjustment of the missile's motion attitude. MAECM expands the application of metastructures in the aerospace field and provides a novel method for designing multifunctional metastructures.
期刊介绍:
Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to:
• The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites
• The control of their environment
• The study of various systems they are involved in, as supports or as targets.
Authors are invited to submit papers on new advances in the following topics to aerospace applications:
• Fluid dynamics
• Energetics and propulsion
• Materials and structures
• Flight mechanics
• Navigation, guidance and control
• Acoustics
• Optics
• Electromagnetism and radar
• Signal and image processing
• Information processing
• Data fusion
• Decision aid
• Human behaviour
• Robotics and intelligent systems
• Complex system engineering.
Etc.