Description: This program is the analytical approach in composite design to determine the safety factors and strength components of a general multidirectional laminate based on the Tsai-Wu failure criterion and also on the first ply failure (FPF) approach by using MATLAB programming. Platform: |
Size: 2048 |
Author:ccwei |
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Description: Laminate analysis of composite plates using Matlab. Based on classical laminated plate theory.-Laminate analysis of composite plates using Matlab. Based on classical laminated plate theory. Platform: |
Size: 99328 |
Author:aritchey |
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Description: 复合材料的优化,内容里边有很好的描述以及很多的计算实例,适合进阶学习-Objective of this Matlab s program was researched optimization analysis of laminated composite plates for determined the ultimate strength and stress effects of plate s under the regular and uniform out-loads. Therefore, generally Reissner s flat and thick shell finite element model (4Node-20Dof) was developed with first-order shear deformation theory (FSDT).
Kirchhoff s classical laminate plate theory yields in adequate results for thick plates (a/th<20). This classical laminated plate (CLPT or CPT), was one of the first developed by Reissner with shear deformation theory. Afterwards, Mindlin was utulizated this shear deformation theory to accommodate rotary of inertia terms on per unit freedom. If this plate system s be very thick (a/th<10) than it is fail to shear deformation-motion and it s condition of adaptive shear stress on plate s top and bottom surface.
While this conditions was produced on plate s segment when requered the shear correction factor of shear locking eff Platform: |
Size: 857088 |
Author:陈浩 |
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Description: 这是关于用MATLAB编写M文件求复合材料层合板性能指标的一个作业，第一个M文件是对层合板性能的分析，第二个M文件是对层合板破坏的分析。-This is written in MATLAB M-file on demand using composite laminates performance of a job, the first M-file is a performance analysis of laminated plates, the second M-file is damaged laminate analysis. Platform: |
Size: 4096 |
Author:qiwuchao |
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Description: 计算层合板刚度，和最先一层失效载荷！程序具有通用性，能够对任意工程弹性常数和几何尺寸的层合板进行刚度和强度分析！非常适合最为哈尔滨工业大学复合材料与工程专业的复合材料力学上机大作业-Laminate stiffness calculation, and the first layer of failure load! Program is versatile, capable of any engineering elastic constants and geometry of laminates for stiffness and strength analysis! Very suitable for most Harbin Institute of Technology composite materials and engineering mechanics of composite materials on the plane big job Platform: |
Size: 1024 |
Author:yuan |
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Description: 本程序用于计算复合材料层合板首层失效强度以及极限强度。-This procedure is used to calculate the composite laminate failure strength and ultimate strength of the first floor. Platform: |
Size: 1024 |
Author:huzheng |
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Description: 层合板，4层，用MATLAB进行编程，然后进行应力应变分析，最后得到失效强度-Laminate, 4 layers, using MATLAB programming, then the stress and strain analysis, and finally get failure intensity Platform: |
Size: 456704 |
Author:大田菜 |
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Description: Calculate A,B,D matrices of composite laminate for random ply angle and represent diagrams of effective laminate properties vs ply angle. Platform: |
Size: 2048 |
Author:FOTIS CHATZIS |
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