Crack detection and localization in composite plates by intersection of first three normalized mode shape curves from experimental modal analysis

Rama Krishna Shinagam, Deepak Raj Kumar Vengalasetti, Tarun Maruvada
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Abstract

Purpose This study aims to identify the location of cracks in composite plates using a normalized mode shape curve algorithm. Crack in any structure is a destructive occurrence. Detecting these cracks early is pivotal for ensuring safety and preventing potential accidents. To prevent failure of structures, it is crucial to detect these cracks effectively and take the necessary precautions. Hence, crack detection and localization techniques are used to avoid sudden failures of structures while in operation. Design/methodology/approach An experimental modal analysis is conducted on composite plates with and without cracks to determine the natural frequencies and mode shapes. For this purpose, an impact hammer, uniaxial accelerometer and four-channel vibration analyzer are used to find the natural frequencies and mode shapes. Numerical modal analysis is performed on no crack and cracked composite plates using ANSYS software, and these are validated by the experimental modal analysis results. The normalized mode shapes algorithm is trained using test data of the first three natural frequencies collected from numerical modal analysis on different cracked composite plates for localization of crack. Findings The natural frequencies derived from both experimental modal analysis and numerical modal analysis exhibit a variance of 9.6%. The estimation of the crack location is achieved with exceptional precision by intersecting the first three normalized mode shapes. The first three normalized mode shape curve intersections provide a solid indication of the crack’s location. As the difference in error between the actual and estimated crack locations is only 0.9%. Originality/value This study introduces the first application of experimental modal analysis in conjunction with the normalized mode shape curve algorithm for localizing cracks in composite plates. The normalization process of mode shapes, derived from experimental modal analysis, forms a fundamental component of the mode shape curve algorithm specifically designed for crack localization. Combining experimental modal analysis with a specific algorithm of normalizing mode shapes is used to identify and locate cracks within these composite plates.
通过实验模态分析的前三条归一化模态振型曲线的交集来检测和定位复合材料板中的裂纹
目的 本研究旨在利用归一化模态振型曲线算法确定复合材料板中裂纹的位置。任何结构出现裂缝都会造成破坏。及早发现这些裂缝对于确保安全和防止潜在事故至关重要。为防止结构失效,有效检测这些裂缝并采取必要的预防措施至关重要。因此,裂纹检测和定位技术被用来避免结构在运行过程中突然失效。设计/方法/途径对有裂纹和无裂纹的复合板进行实验模态分析,以确定固有频率和模态振型。为此,使用了冲击锤、单轴加速度计和四通道振动分析仪来确定固有频率和模态振型。使用 ANSYS 软件对无裂纹和有裂纹的复合板进行了数值模态分析,并通过实验模态分析结果进行了验证。利用从不同裂纹复合板的数值模态分析中收集的前三个固有频率的测试数据,对归一化模态振型算法进行了训练,以确定裂纹的位置。通过与前三个归一化模态振型相交,可以非常精确地估算出裂纹位置。前三个归一化模态振型曲线的交点为裂缝位置提供了可靠的指示。本研究首次将实验模态分析与归一化模态振型曲线算法相结合,用于确定复合板裂纹的位置。由实验模态分析得出的模态振型归一化过程是专为裂纹定位设计的模态振型曲线算法的基本组成部分。将实验模态分析与特定的模态振型归一化算法相结合,可用于识别和定位这些复合材料板中的裂纹。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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