首页> 外文期刊>Arabian Journal for Science and Engineering. Section A, Sciences >Computational Fluid Dynamics Analysis of Moisture Ingress in Aircraft Structural Composite Materials
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Computational Fluid Dynamics Analysis of Moisture Ingress in Aircraft Structural Composite Materials

机译:飞机结构复合材料中水分进入的计算流体动力学分析

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Moisture in composite materials has been proven to be an important issue leading to significant deterioration of commercial aircraft wing structures. Lingering problems associated with this issue that is initiated with defects during manufacturing and finishing include delamination, de-bonding, potential fracture, debris, etc. Despite extensive investigation and refinement in structural design, the water ingress problem persists as no general mitigation technique has yet been developed. Developing sustainable solutions to the water ingress problem can be very time-consuming and costly. The increasing use of composites in the aviation industry and in, for example, honeycomb sandwich components highlights the significant need to address the moisture ingress problem and develop deeper insights which can assist in combating this problem. Experimental testing, although the most dependable approach, can take months, if not years. Numerical simulations provide a powerful and alternative approach to experimental studies for obtaining an insight into the mechanisms and impact of moisture ingress in aircraft composites. The principal advantage is that they can be conducted considerably faster, are less costly than laboratory testing and furthermore can also utilize the results of laboratory studies to aid in visualizing practical problems. Therefore, the present study applies a computational fluid dynamics (CFD) methodology, specifically ANSYS finite volume software and the three fluid-based solvers, Fluent, CFX and ANSYS fluid-structure interaction, to simulate water ingress in composite aerospace structures. It is demonstrated that ANSYS Fluent is a satisfactory computational solver for fundamental studies, providing reasonably accurate results relatively quickly, especially while simulating two-dimensional components. Three-dimensional components are ideally simulated on CFX, although the accuracy achievable is reduced. The structural-fluid-based solver, ANSYS FSI (fluid-structure interaction), unfortunately does not fully implement the material studied leading to reduced accuracy. The simulations reveal interesting features associated with different inlet velocities, inlet fastener hole numbers, void number and dimensions. Pressure, velocity, streamline, total deformation and normal stress plots are presented with extensive interpretation. Furthermore, some possible mitigation pathways for water ingress effects including hydrophobic coatings are outlined.
机译:复合材料中的水分已被证明是导致商用飞机机翼结构显着恶化的重要问题。与该问题相关的挥之不去的问题是由制造和精加工过程中的缺陷引发的,包括分层,脱胶,潜在的断裂,碎屑等。尽管对结构设计进行了广泛的研究和改进,但由于尚未有通用的缓解技术,进水问题仍然存在已开发。针对水进入问题开发可持续的解决方案可能非常耗时且成本高昂。复合材料在航空业和例如蜂窝夹心组件中的使用越来越多,这突出表明了解决湿气进入问题和开发更深层次的见解以解决这一问题的迫切需求。实验测试虽然是最可靠的方法,但可能需要数月甚至数年的时间。数值模拟为实验研究提供了一种有力且可替代的方法,用于深入了解航空复合材料中水分进入的机理和影响。主要优点是,与实验室测试相比,它们可以进行得更快,成本更低,而且还可以利用实验室研究的结果来帮助可视化实际问题。因此,本研究应用计算流体动力学(CFD)方法,特别是ANSYS有限体积软件和基于流体的三个解算器Fluent,CFX和ANSYS流固耦合来模拟复合航空结构中的水进入。事实证明,ANSYS Fluent是基础研究的令人满意的计算求解器,可以相对快速地提供合理准确的结果,尤其是在模拟二维分量时。理想情况下,在CFX上模拟三维组件,尽管降低了可达到的精度。不幸的是,基于结构流体的求解器ANSYS FSI(流体-结构相互作用)不能完全实现所研究的材料,从而导致精度降低。模拟显示了与不同的入口速度,入口紧固件孔数,空隙数和尺寸相关的有趣特征。压力,速度,流线,总变形和法向应力图都有详尽的解释。此外,概述了一些可能的缓解水浸效果的途径,包括疏水涂层。

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