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相关概念视频

Fatigue01:21

Fatigue

782
Fatigue occurs when materials rupture under repeated or fluctuating loads, even at stress levels far below their static breaking strength. It typically results in brittle failure, even for ductile materials. It is a critical consideration in designing machines and structural components subjected to repetitive or varying loads. The nature of these loadings can range from fluctuating loads like unbalanced pump impellers causing vibrations to repeatedly bending a thin steel rod wire back and forth...
782
Relative Motion Analysis using Rotating Axes - Acceleration01:22

Relative Motion Analysis using Rotating Axes - Acceleration

730
Consider a component AB undergoing a linear motion. Along with a linear motion, point B also rotates around point A. To comprehend this complex movement, position vectors for both points A and B are established using a stationary reference frame. The absolute velocity of point B is determined by adding the absolute velocity of point A, the relative velocity of point B in the rotating frame, and the effects caused by the angular velocity within the rotating frame.
Time differentiation is...
730
Stress Concentrations in Circular Shafts01:18

Stress Concentrations in Circular Shafts

516
Consider the elastic torsion formula, which applies to a circular shaft with a consistent cross-section. This formula assumes that the shaft's ends are loaded with rigid plates firmly attached. However, in many cases, torques are applied to the shaft through mechanisms like flange couplings or gears, which are connected by keys inserted into keyways. This application method modifies the stress distribution near the point of torque application, causing it to deviate from the distributions...
516
Deformation in a Circular Shaft01:10

Deformation in a Circular Shaft

816
One of the distinctive characteristics of circular shafts is their ability to maintain their cross-sectional integrity under torsion. In other words, each cross-section continues to exist as a flat, unaltered entity, simply rotating like a solid, rigid slab. To understand the distribution of shearing stress within such a shaft, consider a cylindrical section inside this circular shaft. This section has a length of L and a radius of R, with one end fixed. The radius of the cylindrical section is...
816
Mohr's Circle for Plane Strain01:18

Mohr's Circle for Plane Strain

1.1K
Mohr's circle is a crucial graphical method used to analyze plane strain by plotting strain on a set of cartesian coordinates, where the abscissa is normal strain ∈ and the ordinate is shear strain γ. Similarly to Mohr’s circle for plane stress, two points X and Y are plotted. Their coordinates are (∈x, -γXY) and (∈Y, γXY), respectively.
Mohr's circle visually represents the strain states under various conditions, which is essential for...
1.1K
Residual Stresses in Circular Shafts01:10

Residual Stresses in Circular Shafts

497
In materials that exhibit elastic and plastic behavior, known as elastoplastic materials, residual stresses can accumulate when these materials experience plastic deformation. This deformation arises from either high levels of shearing stress or significant strains. Residual stresses are internal stresses that persist within a material after removing the external force causing deformation. This phenomenon is demonstrated when observing the behavior of a shaft under torque; notably, the...
497

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Updated: Jan 10, 2026

Full-field Strain Measurements for Microstructurally Small Fatigue Crack Propagation Using Digital Image Correlation Method
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一种只有加速的模态循环配套方法,用于现场疲劳损伤检测.

Da Som Kang1, Seung-Hoon Bae2, Seunghun Baek3

  • 1Aero Business Group, Hanwha Aerospace, Seongnam, 13488, South Korea.

Scientific reports
|November 29, 2025
PubMed
概括

一种新的模态循环装配技术从振动数据中估计了自然频率和阻尼比. 这种方法可以检测航空航天领域的早期疲劳损伤,通过频率转移和分峰模式来表明这一点.

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Full-field Strain Measurements for Microstructurally Small Fatigue Crack Propagation Using Digital Image Correlation Method
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Crack Monitoring in Resonance Fatigue Testing of Welded Specimens Using Digital Image Correlation
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科学领域:

  • 结构动力学 结构动力学
  • 机械工程 机械工程
  • 航空航天工程 航空航天工程

背景情况:

  • 模式分析对于理解结构性行为至关重要.
  • 检测早期疲劳损伤对于结构完整性和安全至关重要.
  • 对于非破坏性测试,只有输出模式识别方法是可取的.

研究的目的:

  • 引入一种用于模态参数估计的新型模态循环拟合方法.
  • 为了验证该方法在检测疲劳损伤方面的有效性.
  • 建立关键指标,用于识别航空航天结构中的非可见疲劳.

主要方法:

  • 开发一种模态循环适配算法,用于自然频率和减噪比率的估计.
  • 仅使用输出加速度测量.
  • 在航空航天支架样本上使用振动疲劳测试进行实验验证.

主要成果:

  • 从加速数据中成功估计了自然频率和减缓比.
  • 检测初始的,不可见的疲劳损伤.
  • 在随机振动刺激下观察到自然频率的下降.
  • 在正弦刺激下,频率响应函数中出现"分裂峰值"模式.

结论:

  • 拟议的模态循环配合方法对于仅输出模态识别是有效的.
  • 该方法可以可靠地检测航空航天部件的早期疲劳损伤.
  • 特定的振动信号 (频率下降,分峰) 作为疲劳损伤的指标.