高纵横比复合材料机翼:几何非线性气动弹性、多学科设计优化、制造和实验测试

T. Farsadi, Majid Ahmadi, Melin Sahin, H. Haddad Khodaparast, A. Kayran, M.I. Friswell
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摘要

在航空航天工程领域,高纵横比复合材料机翼的设计和制造已成为创新和效率的焦点。这些细长的机翼由碳纤维等先进材料制成,并采用真空袋等高效制造方法,有望大幅减轻飞机重量、降低油耗并提高整体性能。然而,要充分实现这些优势,必须解决结构和气动弹性方面的诸多限制。本研究提出了一种新颖的气动量身定制的多目标、多学科优化设计(MMDO)方法,该方法无缝集成了数值优化技术,可最大限度地减轻重量并确保结构完整性。然后制造优化后的机翼配置,并使用地面振动试验(GVT)和数字图像相关(DIC)系统进行静态挠度分析,以验证数值模型并与之相关联。在全自动内部非线性气动弹性模拟软件(NAS2)软件包(版本 v1.0)中,分析工具的集成提供了一种强大的数值方法,用于提高复合材料机翼设计的气动弹性和结构性能。其中包括非线性气动弹性分析和裁剪,以及基于群体的随机优化,以确定 NAS2 中的最佳设计。这些分析工具为设计具有更佳气动弹性和结构特性的复合材料机翼提供了全面、高效的方法。这种综合方法旨在生产出不仅符合严格的安全和性能标准,而且还能提高航空航天工业成本效益的复合材料机翼。通过这种多学科方法,作者试图强调气动弹性解决方案在高纵横比复合材料机翼的先进设计和制造中的关键作用,从而为航空航天技术的持续发展做出贡献。
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High Aspect Ratio Composite Wings: Geometrically Nonlinear Aeroelasticity, Multi-Disciplinary Design Optimization, Manufacturing, and Experimental Testing
In the field of aerospace engineering, the design and manufacturing of high aspect ratio composite wings has become a focal point of innovation and efficiency. These long, slender wings, constructed with advanced materials such as carbon fiber and employing efficient manufacturing methods such as vacuum bagging, hold the promise of significantly lighter aircraft, reduced fuel consumption, and enhanced overall performance. However, to fully realize these benefits, it is imperative to address a multitude of structural and aeroelastic constraints. This research presents a novel aeroelastically tailored Multi-objective, Multi-disciplinary Design Optimization (MMDO) approach that seamlessly integrates numerical optimization techniques to minimize weight and ensure structural integrity. The optimized wing configuration is then manufactured, and a Ground Vibration Test (GVT) and static deflection analysis using the Digital Image Correlation (DIC) system are used to validate and correlate with the numerical model. Within the fully automated in-house Nonlinear Aeroelastic Simulation Software (NAS2) package (version v1.0), the integration of analytical tools offers a robust numerical approach for enhancing aeroelastic and structural performance in the design of composite wings. Nonlinear aeroelastic analyses and tailoring are included, and a population-based stochastic optimization is used to determine the optimum design within NAS2. These analytical tools contribute to a comprehensive and efficient methodology for designing composite wings with improved aeroelastic and structural characteristics. This comprehensive methodology aims to produce composite wings that not only meet rigorous safety and performance standards but also drive cost-efficiency in the aerospace industry. Through this multidisciplinary approach, the authors seek to underscore the pivotal role of tailoring aeroelastic solutions in the advanced design and manufacturing of high aspect ratio composite wings, thereby contributing to the continued evolution of aerospace technology.
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