BİR HAVACILIK ELASTOPLASTİK YAPISAL DELİKLİ SİLİNDİRİK BİLEŞENİN DÖNGÜSEL MEKANİK YÜK ALTINDA COMSOL MULTIPHYSICS VE TAGUCHI METODU OPTİMİZASYONU İLE YORULMA ANALİZİ

Erkan Tur
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Abstract

This research study focuses on the fatigue behavior of an aerospace elastoplastic cylindrical structural component with a hole subjected to cyclic mechanical loads. In the demanding operational environment of aerospace applications, the structural components, particularly those with stress concentrators like holes, experience cyclic loading conditions, leading to fatigue failure over time. The key objective of this study is to gain insights into this fatigue behavior, and to develop an optimized set of design and operational parameters that can enhance the fatigue performance of these components. Utilizing the robust finite element analysis capabilities of COMSOL Multiphysics, a comprehensive model of the elastoplastic cylindrical component is developed. The model captures the intricate effects of the hole, a typical stress raiser, on the fatigue performance under various cyclic mechanical loading conditions. A detailed fatigue analysis is then performed using this model, providing valuable insights into the fatigue life and failure patterns of the component. To enhance the fatigue performance, the Taguchi method, a statistical approach, is employed. This method helps to identify and optimize the key design and operational parameters influencing the fatigue life. The parameters are optimized based on their signal-to-noise ratio, with an aim to maximize the fatigue life and ensure the structural integrity of the component under operational cyclic loads. The findings of this research hold significant implications for the design and manufacturing of aerospace structural components, with potential benefits of improved safety, enhanced durability, and reduced maintenance requirements. However, the results' applicability might be limited by the complexity of real-world operational conditions and the assumptions made in the simulation model. Future studies can validate and enhance these results by incorporating more complex loading scenarios and real-world case studies.
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利用 comsol 多物理场和塔口法优化对循环机械载荷下的航空弹性塑料结构穿孔圆筒部件进行疲劳分析
本研究的重点是带孔的航空弹性塑料圆柱形结构组件在承受循环机械载荷时的疲劳行为。在要求苛刻的航空航天应用操作环境中,结构组件,尤其是那些带有孔洞等应力集中点的结构组件,会经历循环加载条件,从而导致疲劳失效。本研究的主要目的是深入了解这种疲劳行为,并开发一套优化的设计和运行参数,以提高这些部件的疲劳性能。利用 COMSOL Multiphysics 强大的有限元分析功能,开发了弹性圆柱形组件的综合模型。该模型捕捉到了孔这个典型的应力提升器在各种循环机械加载条件下对疲劳性能的复杂影响。然后利用该模型进行了详细的疲劳分析,为了解部件的疲劳寿命和失效模式提供了宝贵的信息。为了提高疲劳性能,采用了田口方法(一种统计方法)。该方法有助于确定和优化影响疲劳寿命的关键设计和操作参数。参数的优化基于其信噪比,目的是最大限度地延长疲劳寿命,并确保部件在工作循环载荷下的结构完整性。这项研究成果对航空航天结构部件的设计和制造具有重要意义,可提高安全性、增强耐用性并降低维护要求。然而,由于真实世界运行条件的复杂性和模拟模型中的假设,研究结果的适用性可能会受到限制。未来的研究可以通过纳入更复杂的加载场景和实际案例研究来验证和增强这些结果。
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