2023
DOI: 10.1016/j.tws.2022.110491
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Improved mechanical characteristics of new auxetic structures based on stretch-dominated-mechanism deformation under compressive and tensile loadings

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Cited by 23 publications
(4 citation statements)
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“…These values are calculated based on the size of the structure before deformation, and normal stress ε is not a localized stress that directly acts on the structure, but rather represents an overall equivalent stress. The definitions for normal stress σ and normal strain ε are as follows: [ 27,28,36 ] σ=FA$$\sigma = \frac{F}{A}$$ε=ΔHH$$\epsilon = \frac{\Delta H}{H}$$the stress σ and strain ε listed in Equation () and () belong to the category of “engineering” stress and strain. Where F represents the reaction force in the impacting end, and A represents the initial cross‐sectional area of the entire structure that is perpendicular to F , and is defined as A = L × b , where b is the thickness of 20 mm in the outward direction of the honeycomb surface, and L and H denote the initial width and initial height of the entire structure, respectively.…”
Section: Designing and Methodsmentioning
confidence: 99%
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“…These values are calculated based on the size of the structure before deformation, and normal stress ε is not a localized stress that directly acts on the structure, but rather represents an overall equivalent stress. The definitions for normal stress σ and normal strain ε are as follows: [ 27,28,36 ] σ=FA$$\sigma = \frac{F}{A}$$ε=ΔHH$$\epsilon = \frac{\Delta H}{H}$$the stress σ and strain ε listed in Equation () and () belong to the category of “engineering” stress and strain. Where F represents the reaction force in the impacting end, and A represents the initial cross‐sectional area of the entire structure that is perpendicular to F , and is defined as A = L × b , where b is the thickness of 20 mm in the outward direction of the honeycomb surface, and L and H denote the initial width and initial height of the entire structure, respectively.…”
Section: Designing and Methodsmentioning
confidence: 99%
“…These values are calculated based on the size of the structure before deformation, and normal stress ε is not a localized stress that directly acts on the structure, but rather represents an overall equivalent stress. The definitions for normal stress σ and normal strain ε are as follows: [27,28,36] σ…”
Section: Normal Stress and Normal Strainmentioning
confidence: 99%
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“…Numerous other studies have utilised FEA to investigate several variations based on the 2D re-entrant hexagonal honeycomb systems and Sigmund's double-V model (Figure 1c-i) to simulate their mechanical properties, including in-plane Poisson's ratio and Young's modulus under uniaxial loading [135][136][137][138][139]. Through FEA simulations, several studies were carried out on the shape optimization of the re-entrant honeycombs by analysing the effect of a number of variables on the physical properties.…”
Section: Two Dimensional Systemsmentioning
confidence: 99%