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Development of the detonation-driven expansion tube for orbital speed experiments
Jiang ZL(姜宗林); Wu B(吴波); Gao YL; Zhao W(赵伟); Hu ZM(胡宗民); Jiang, ZL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
发表期刊Science China-Technological Sciences
2015-04
卷号58期号:4页码:695-700
ISSN1674-7321
摘要The hypersonic flow at orbital speeds is a fundamental issue for the ground tests of aerospace crafts. The detonation-driven high-enthalpy expansion tube (JF16 expansion tube) was developed to investigate re-entry physics. A forward detonation cavity (FDC) driver was applied in the JF16 expansion tube to create stable driving flows. The sound speed ratio of the detonated to test gas was examined to minimize the magnitude of test flow perturbations. The acceleration section length, incident shock decay and diaphragms thickness were investigated in detail to obtain optimal operation parameters. Flow visualization was also carried out with schlieren system to demonstrate the test flow stability and the effective test duration. Experimental data showed that the test flow with a velocity of 8.3 km/s and a total enthalpy up to 40 MJ/kg can be generated successfully and the test duration lasts for more than 50 mu s.
关键词Detonation Driver Shock-expansion Tube High-enthalpy Flow Test Flow
学科领域Engineering, Multidisciplinary ; Materials Science, Multidisciplinary
DOI10.1007/s11431-014-5756-1
URL查看原文
收录类别SCI ; EI ; CSCD
语种英语
WOS记录号WOS:000351861900012
关键词[WOS]HIGH-ENTHALPY
WOS研究方向Engineering ; Materials Science
WOS类目Engineering, Multidisciplinary ; Materials Science, Multidisciplinary
项目资助者National Natural Science Foundation of China [10632090, 10621202]
课题组名称LHD激波与爆轰物理
论文分区二类/Q2
引用统计
被引频次:6[WOS]   [WOS记录]     [WOS相关记录]
文献类型期刊论文
条目标识符http://dspace.imech.ac.cn/handle/311007/49914
专题高温气体动力学国家重点实验室
通讯作者Jiang, ZL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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GB/T 7714
Jiang ZL,Wu B,Gao YL,et al. Development of the detonation-driven expansion tube for orbital speed experiments[J]. Science China-Technological Sciences,2015,58,4,:695-700.
APA 姜宗林,吴波,Gao YL,赵伟,胡宗民,&Jiang, ZL .(2015).Development of the detonation-driven expansion tube for orbital speed experiments.Science China-Technological Sciences,58(4),695-700.
MLA 姜宗林,et al."Development of the detonation-driven expansion tube for orbital speed experiments".Science China-Technological Sciences 58.4(2015):695-700.
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