Numerical investigation of the axial impulse load during the startup in the shock tunnel

doi:10.1016/j.ast.2017.12.013

CORC > 力学研究所 > 中国科学院力学研究所 > 高温气体动力学国家重点实验室

	Numerical investigation of the axial impulse load during the startup in the shock tunnel
	Meng BQ(孟宝清); Han GL(韩桂来); Luo ZT(罗长童); Jiang ZL(姜宗林)
刊名	AEROSPACE SCIENCE AND TECHNOLOGY
	2018-02-01
卷号	73 页码:332-342
关键词	Hypersonic Shock tunnel Start-up process Impulse force Vibration
ISSN号	1270-9638
DOI	10.1016/j.ast.2017.12.013
英文摘要	A shock tunnel is a representative type of ground-based equipment in the hypersonic field, which has the advantage of free stream of excellent quality. Accurate measurements of aerodynamic forces in the shock tunnel are great challenges. The impulse loads during the start-up process induce the vibration of the model and its support. Aerodynamic signals are disturbed by vibrational signals. The identification of the starting time of the steady periodic vibration and excited natural frequencies of the whole structure would contribute to improve the accuracy of measurement. These two factors are closely related to the properties of the impulse forces. However, there is currently no published research on the impulse forces. In this paper, the type of impulse forces (drag history) acting on the sharp cone during the start-up process was investigated by numerical simulation. The distribution of the static pressure of the typical wave structures was found to have a significant influence on the types of the drag history. A formula, based on the physical analysis of start-up process, was put forward to estimate the starting time of the steady stage. Additionally, the subsequent analysis and design optimization such as vibration of structure and disturbing frequencies needed an analytical and simple formation of drag history. Thus, the drag history was approximated by numbers of sine functions. Different phases exhibited notable difference in composition. Also, a metric denoted as the energy coefficient was derived to identify the critical frequencies and simplify the analytical expression of the impulse force. (C) 2017 Elsevier Masson SAS. All rights reserved.
分类号	一类
URL标识	查看原文
WOS关键词	FORCE BALANCE ; NOZZLE ; DESIGN
WOS研究方向	Engineering, Aerospace
语种	英语
WOS记录号	WOS:000424185200029
资助机构	National Natural Science Foundation of China [11472281, 11532014] ; National Key Program of Research and Development [2016YFA0401200]
内容类型	期刊论文
源URL	[http://dspace.imech.ac.cn/handle/311007/77884]
专题	力学研究所_高温气体动力学国家重点实验室
作者单位	1.Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China 2.Univ Chinese Acad Sci, Beijing 100049, Peoples R China
推荐引用方式 GB/T 7714	Meng BQ,Han GL,Luo ZT,et al. Numerical investigation of the axial impulse load during the startup in the shock tunnel[J]. AEROSPACE SCIENCE AND TECHNOLOGY,2018,73:332-342.
APA	孟宝清,韩桂来,罗长童,&姜宗林.(2018).Numerical investigation of the axial impulse load during the startup in the shock tunnel.AEROSPACE SCIENCE AND TECHNOLOGY,73,332-342.
MLA	孟宝清,et al."Numerical investigation of the axial impulse load during the startup in the shock tunnel".AEROSPACE SCIENCE AND TECHNOLOGY 73(2018):332-342.