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Titlebook: A Numerical Approach to the Micromechanics of Fibre-Reinforced Laminae; The Micromechanics A Andreas ?chsner,Resam Makvandi Book 2024 The E

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發(fā)表于 2025-3-21 18:18:32 | 只看該作者 |倒序瀏覽 |閱讀模式
期刊全稱A Numerical Approach to the Micromechanics of Fibre-Reinforced Laminae
期刊簡稱The Micromechanics A
影響因子2023Andreas ?chsner,Resam Makvandi
視頻videohttp://file.papertrans.cn/168/167049/167049.mp4
發(fā)行地址Provides numerical solutions to model the micromechanics of laminae.Includes a Python-based computational tool to easily predict the elastic properties.Approaches the elasticity solutions with contigu
學科分類Advanced Structured Materials
圖書封面Titlebook: A Numerical Approach to the Micromechanics of Fibre-Reinforced Laminae; The Micromechanics A Andreas ?chsner,Resam Makvandi Book 2024 The E
影響因子.This book treats the micromechanics of laminae, i.e., the prediction of the macroscopic mechanical lamina properties based on the mechanical properties of the constituents, i.e., fibers and matrix. The focus is on unidirectional lamina which can be described based on orthotropic constitutive equations. In detail, predictions for the modulus of elasticity in and transverse to the fiber direction, the major Poisson’s ratio, as wells as the in-plane shear modulus are provided. The mechanics of materials approach, the elasticity solutions with contiguity after Tsai, and the Halpin-Tsai relationships, are presented in detail...Composite materials, especially fiber-reinforced composites, are gaining increasing importance since they can overcome the limits of many structures based on classical engineering materials. Particularly the combination of a matrix with fibers provides far better properties than the single constituents alone. A typical basic layer, the so-called lamina, can be composed of unidirectional fibers which are embedded in a matrix. In a second step, layers of laminae may be stacked under different fiber angles to a so-called laminate, which reveals—depending on the stac
Pindex Book 2024
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沙發(fā)
發(fā)表于 2025-3-21 23:57:45 | 只看該作者
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發(fā)表于 2025-3-22 04:23:16 | 只看該作者
Grundprinzip des Grundeinkommens,l, predictions for the modulus of elasticity in and transverse to the fiber direction, the major Poisson’s ratio as well as the in-plane shear modulus are provided. The mechanics of materials approach, the elasticity solutions with contiguity after Tsai, and the Halpin-Tsai relationships are presented in detail.
地板
發(fā)表于 2025-3-22 07:36:26 | 只看該作者
Introduction, fibers. The second part of this chapter introduces the concept of reference numbers, which are commonly used to predict and characterize the properties of composites depending on their composition. The common approaches are related to the volume, mass, or relative density.
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發(fā)表于 2025-3-22 09:36:40 | 只看該作者
Prediction of Elastic Properties of Laminae,l, predictions for the modulus of elasticity in and transverse to the fiber direction, the major Poisson’s ratio as well as the in-plane shear modulus are provided. The mechanics of materials approach, the elasticity solutions with contiguity after Tsai, and the Halpin-Tsai relationships are presented in detail.
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發(fā)表于 2025-3-22 17:53:25 | 只看該作者
Introduction,operties than a single component for itself. The focus is on fiber-reinforced composites where a single layer has unidirectionally aligned reinforcing fibers. The second part of this chapter introduces the concept of reference numbers, which are commonly used to predict and characterize the properti
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發(fā)表于 2025-3-22 21:46:09 | 只看該作者
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發(fā)表于 2025-3-23 03:58:07 | 只看該作者
,Micromechanics Analysis Tool—MMAT v1.0,. The choices for the different tools and libraries, particularly for our user interface, are explained in detail. The second part of this chapter covers the graphical appearance, functionality, and the practical handling of MMAT v1.0.
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發(fā)表于 2025-3-23 09:11:05 | 只看該作者
Application Examples,esult plots or tables obtained in CLAT 1D. The presented problems comprise the calculation of stresses and strains in symmetric and asymmetric laminates, the application of failure criteria, and the ply-by-ply failure of laminates.
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