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相关概念视频

Unsymmetric Loading of Thin-Walled Members: Problem Solving01:07

Unsymmetric Loading of Thin-Walled Members: Problem Solving

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The shear center of a channel section with uniform thickness, height, and width, is determined by computing the shear force in the member and calculating the moments of inertia of the sections.
To compute the shear forces, find the shear flow at a specific distance from the endpoint using the vertical shear and the moment of inertia values. The total shear force on the flange is calculated by integrating the shear flow from one end of the flange to the other.
Next, calculate the moments of...
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Bending of Members Made of Several Materials01:11

Bending of Members Made of Several Materials

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In analyzing a structural member composed of two different materials with identical cross-sectional areas, it is crucial to understand how their distinct elastic properties affect the member's response under load. The analysis involves assessing stress and strain distributions using the transformed section concept, which accounts for variations in material properties.
Hooke's Law determines stress in each material, stating that stress is proportional to strain but varies due to each material's...
659
Unsymmetric Loading of Thin-Walled Members01:23

Unsymmetric Loading of Thin-Walled Members

465
Thin-walled members with non-symmetrical cross-sections are vital to engineering structures, offering material efficiency and structural integrity. However, unsymmetrical loading on these members leads to complex stress distributions, resulting in simultaneous bending and twisting can cause deformation or structural failure. The interaction between bending and twisting requires detailed analysis to ensure structural resilience.
The concept of the shear center is crucial in countering the...
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Shear and Bending Moment Diagram: Problem Solving01:24

Shear and Bending Moment Diagram: Problem Solving

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When analyzing a beam supporting concentrated loads and a distributed load, drawing the shear and bending moment diagrams is essential. These diagrams help understand the internal forces and moments acting on the beam, which is crucial for designing safe and efficient structures. Follow these steps to create the shear and bending moment diagrams:
Draw a Free-Body Diagram: Start by drawing a free-body diagram of the entire beam, including the concentrated loads, distributed load, and reaction...
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Determination of Pi Terms01:15

Determination of Pi Terms

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The Buckingham Pi theorem is a valuable method in dimensional analysis, reducing complex relationships between variables into dimensionless terms. Relevant variables in analyzing the lift force on an airplane wing include lift force, air density, wing area, aircraft velocity, and air viscosity. Expressing each variable in terms of fundamental dimensions — mass, length, and time — provides a consistent foundation for constructing these dimensionless terms.
The theorem indicates that the...
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Method of Superposition01:20

Method of Superposition

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The method of superposition is a crucial technique in structural engineering, used to analyze the effect of multiple loads on beams. This approach involves calculating the deflection and slope for each load on a beam separately, and then summing these effects to determine the overall impact. It is applicable only when the beam material remains within its elastic limit, ensuring that deformations are linearly elastic.
When applying the method of superposition, each type of load—whether...
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相关实验视频

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使用多补丁参数化和基于罚款的合方法对翼结构进行异地测量分析.

Dawei Wang1, Xian Cao1, Yang Xue1

  • 1COMAC Beijing Aircraft Technology Research Institute, Beijing, 102211, China.

Scientific reports
|March 6, 2026
PubMed
概括

本研究引入了使用异地形分析 (IGA) 的飞机机翼的新几何参数化. 与传统的有限元素分析 (FEA) 相比,IGA在使用较少的计算资源实现了高精度.

关键词:
分析 - 适合分析.几何参数化的几何参数化异地质分析分析.基于罚款的合方式莱斯纳明德林贝理论理论机翼结构结构 机翼结构 机翼结构

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科学领域:

  • 航空航天工程 航空航天工程
  • 计算力学 计算力学 计算力学
  • 结构分析 结构分析

背景情况:

  • 在飞机设计中,几何参数化和结构分析至关重要.
  • 与传统的有限元素方法 (FEM) 相比,同位几何分析 (IGA) 提供了更高的准确性和简化CAD/CAE集成.

研究的目的:

  • 为经典飞机机翼结构开发一个分析适合的几何参数化.
  • 为了验证IGA对复杂飞机机翼分析的有效性.

主要方法:

  • 使用非统一的理性B-splines (NURBS) 来进行多补丁翼几何表示.
  • 在IGA框架内应用Reissner-Mindlin外理论.
  • 实施了针对不符合接口连续性的基于惩罚的方法.
  • 进行静态曲分析,并将结果与ABAQUS中的常规FEM进行比较.

主要成果:

  • 为飞机机翼结构开发了一个符合规范的几何参数化.
  • IGA的结果与FEA的参考解决方案有很好的一致性.
  • 实现了与FEA相似的精度,自由度显著降低.

结论:

  • 拟议的IGA方法对于飞机机翼结构分析非常有效.
  • 对于复杂的航空航天结构,IGA为传统的FEA提供了一个计算效率高的替代方案.