Evolution of temporal features during pyroshock propagation caused by wave dispersion

IF 5.8 1区 工程技术 Q1 ENGINEERING, AEROSPACE Aerospace Science and Technology Pub Date : 2025-02-01 Epub Date: 2024-12-06 DOI:10.1016/j.ast.2024.109841
Jianbin Ruan , Yinzhong Yan , Pu Xue , Yulong Li
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Abstract

Aerospace devices are vulnerable to pyroshock and require testing. The shock response spectrum (SRS) compares shock severity but ignores temporal features. To improve testing reliability, temporal characteristics and their changes during pyroshock propagation need to be studied. In this paper, the shock propagation problem is studied experimentally. Two temporal features, i.e., the effective duration and the initial rise time, are characterized by the moving mean square method. An appropriate window length is suggested based on the frequency analysis of the shock environment. The evolutions of the effective duration and the initial rise time are characterized and traced during shock propagation. The elastic wave mode of shock propagation is analyzed. It is found that shock propagates in structures mainly in the form of flexural mode. A temporal features prediction method based on traveling damped sine waves is also provided and validated by experimental results.
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波频散引起的热激波传播过程中时间特征的演化
航空航天设备容易受到热冲击,需要进行测试。冲击反应谱(shock response spectrum, SRS)比较冲击的严重程度,但忽略了时间特征。为了提高测试的可靠性,需要研究热激波传播过程中的时间特性及其变化。本文对激波传播问题进行了实验研究。用移动均方法对有效持续时间和初始上升时间两个时间特征进行表征。根据冲击环境的频率分析,提出了合适的窗长。对冲击传播过程中有效持续时间和初始上升时间的演变进行了表征和跟踪。分析了冲击传播的弹性波模式。研究发现,冲击在结构中主要以弯曲模态传播。提出了一种基于行阻尼正弦波的时间特征预测方法,并通过实验验证了该方法的有效性。
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来源期刊
Aerospace Science and Technology
Aerospace Science and Technology 工程技术-工程:宇航
CiteScore
10.30
自引率
28.60%
发文量
654
审稿时长
54 days
期刊介绍: Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to: • The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites • The control of their environment • The study of various systems they are involved in, as supports or as targets. Authors are invited to submit papers on new advances in the following topics to aerospace applications: • Fluid dynamics • Energetics and propulsion • Materials and structures • Flight mechanics • Navigation, guidance and control • Acoustics • Optics • Electromagnetism and radar • Signal and image processing • Information processing • Data fusion • Decision aid • Human behaviour • Robotics and intelligent systems • Complex system engineering. Etc.
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