Sub-scale flight test model design: Developments, challenges and opportunities

IF 11.5 1区 工程技术 Q1 ENGINEERING, AEROSPACE Progress in Aerospace Sciences Pub Date : 2022-04-01 DOI:10.1016/j.paerosci.2021.100798
A. Raju Kulkarni , G. La Rocca, L.L.M. Veldhuis, G. Eitelberg
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引用次数: 6

Abstract

Growing interest in unconventional aircraft designs coupled with miniaturization of electronics and advancements in manufacturing techniques have revived the interest in the use of Sub-scale Flight Testing (SFT) to study the flight behaviour of full-scale aircraft in the early stages of design process by means of free-flying sub-scale models. SFT is particularly useful in the study of unconventional aircraft configurations as their behaviour cannot be reliably predicted based on legacy aircraft designs. In this paper, we survey the evolution of various design approaches (from 1848 to 2021) used to ensure similitude between a sub-scale model and its full-scale counterpart, which is an essential requirement to effectively perform SFT. Next, we present an exhaustive list of existing sub-scale models used in SFT and analyse the key trends in their design approaches, test-objectives, and applications. From this review, we conclude that the state-of-the-art sub-scale model design methods available in literature have not been used extensively in practice. Furthermore, we argue that one sub-scale model is not sufficient to predict the complete flight behaviour of a full-scale aircraft, but a catalog of tailored sub-scale models is needed to predict full-scale behaviour. An introduction to the development of such a catalog is presented in this paper, but the development of a formal methodology remains an open challenge. Establishing an approach to develop and use a SFT catalog of models to predict full-scale aircraft behaviour will help engineers enhance confidence on their designs and make SFT a viable and attractive testing method in the early stages of design.

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亚尺度飞行试验模型设计:发展、挑战和机遇
对非常规飞机设计的兴趣日益增长,加上电子产品的小型化和制造技术的进步,使人们对使用次尺度飞行测试(SFT)的兴趣重新燃起,通过自由飞行的次尺度模型,在设计过程的早期阶段研究全尺寸飞机的飞行行为。SFT在非常规飞机结构的研究中特别有用,因为它们的行为无法根据传统飞机设计可靠地预测。在本文中,我们调查了各种设计方法的演变(从1848年到2021年),用于确保亚尺度模型与其全尺寸模型之间的相似性,这是有效执行SFT的基本要求。接下来,我们给出了SFT中使用的现有亚尺度模型的详尽列表,并分析了其设计方法、测试目标和应用中的关键趋势。从这篇综述中,我们得出结论,文献中最先进的亚尺度模型设计方法尚未在实践中得到广泛应用。此外,我们认为一个亚尺度模型不足以预测全尺寸飞机的完整飞行行为,但需要一个定制的亚尺度模型目录来预测全尺寸飞机的行为。本文介绍了这种目录的发展,但正式方法的发展仍然是一个公开的挑战。建立一种方法来开发和使用SFT模型目录来预测全尺寸飞机的行为,将有助于工程师增强对其设计的信心,并使SFT在设计的早期阶段成为一种可行且有吸引力的测试方法。
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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来源期刊
Progress in Aerospace Sciences
Progress in Aerospace Sciences 工程技术-工程:宇航
CiteScore
20.20
自引率
3.10%
发文量
41
审稿时长
5 months
期刊介绍: "Progress in Aerospace Sciences" is a prestigious international review journal focusing on research in aerospace sciences and its applications in research organizations, industry, and universities. The journal aims to appeal to a wide range of readers and provide valuable information. The primary content of the journal consists of specially commissioned review articles. These articles serve to collate the latest advancements in the expansive field of aerospace sciences. Unlike other journals, there are no restrictions on the length of papers. Authors are encouraged to furnish specialist readers with a clear and concise summary of recent work, while also providing enough detail for general aerospace readers to stay updated on developments in fields beyond their own expertise.
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