用开源软件进行负荷谱分析-一个应用实例

Q4 Engineering
Marek S. Łukasiewicz
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引用次数: 0

摘要

数字实验数据的处理已经成为几乎每一个研究项目的关键部分。随着传感器变得更加多样化和廉价,需要处理的信息量也大大增加。特别是疲劳失效建模,由于其性质需要大量的样品进行处理和可视化。本文基于对无人机飞行中收集的载荷数据的分析。为用例开发并考虑了几个版本的分析程序。每个实现包括摄取数据文件,创建传输数组和“雨流计数”算法。出于易用性和功能性的考虑,选择基于Python编程语言的版本进行呈现。这种方法的开发迭代时间短,可以通过调整参数来更好地表示实际获得的数据,从而获得新的见解。结果和软件本身都可以在网络浏览器中轻松查看,并且无需在本地安装任何软件即可进行修改。开发的软件旨在展示致力于航空航天和机械工程研究的开源计算工具的能力,在这些领域它们仍然相对不受欢迎。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Load Spectrum Analysis with Open Source Software – An Application Example
Abstract Processing of digital experimental data has become a key part of virtually every research project. As sensors get both more diverse and cheaper, the amount of information to be handled greatly increases as well. Especially fatigue failure modelling requires by its nature large numbers of samples to be processed, and visualised. The presented paper is based on analysis of load data gathered in flight on an unmanned aircraft. A few versions of an analysis program were developed and considered for the use case. Each implementation included ingesting the data files, creating transfer arrays and the “rain flow counting” algorithm. For the sake of the ease of use and functionality, the version based on Python programming language was selected for presentation. Short development iteration time of this approach allowed gaining new insights by tweaking parameters to better represent actual acquired data. Both the results and the software itself can be easily viewed in a web browser and run with modifications without the need to install any software locally. The developed software is meant as a demonstration of capabilities of open source computation tools dedicated to aerospace and mechanical engineering research, where they remain relatively unpopular.
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来源期刊
Fatigue of Aircraft Structures
Fatigue of Aircraft Structures Engineering-Safety, Risk, Reliability and Quality
CiteScore
0.40
自引率
0.00%
发文量
0
期刊介绍: The publication focuses on problems of aeronautical fatigue and structural integrity. The preferred topics include: full-scale fatigue testing of aircraft and aircraft structural components, fatigue of materials and structures, advanced materials and innovative structural concepts, damage tolerant design of aircraft structure, life extension and management of ageing fleets, structural health monitoring and loads, fatigue crack growth and life prediction methods, NDT inspections, airworthiness considerations.
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