State-of-the-art Experimental Techniques for VTOL Structural Dynamics

R. Hallez, E. Lorenzo
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Abstract

Increasing complexity in modern aircraft systems and structures makes it challenging for engineers to develop aircraft within time and budget constraints. This is particularly true in the context of new Vertical Take-off and Landing (VTOL) vehicle development where many disruptive aircraft configurations are being studied. Ground and flight testing help to validate aircraft structural dynamic performance and prove that the aircraft meets certification requirements. Several experimental techniques have been developed lately to help getting deeper insight into aircraft structural dynamics and are helpful to accelerate the verification and certification process of new VTOL vehicles. Some of these methods have been recently industrialized and are available in commercial hardware and software solutions. This includes techniques for contactless measurements based on digital image correlation as well as methods for accelerated modal testing and identification of non-linearities in aircraft structures. These methods are presented here and positioned in the context of accelerated VTOL aircraft development.
垂直起降结构动力学的最新实验技术
现代飞机系统和结构日益复杂,使得工程师在时间和预算限制下开发飞机具有挑战性。在新的垂直起降(VTOL)飞行器开发的背景下,这一点尤其正确,许多破坏性的飞机配置正在研究中。地面和飞行测试有助于验证飞机的结构动力性能,并证明飞机符合认证要求。近年来,一些实验技术的发展有助于更深入地了解飞机结构动力学,并有助于加快新型垂直起降飞行器的验证和认证过程。其中一些方法最近已经工业化,并在商业硬件和软件解决方案中可用。这包括基于数字图像相关的非接触式测量技术,以及加速模态测试和飞机结构非线性识别的方法。这些方法在这里提出,并定位在加速垂直起降飞机发展的背景下。
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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