IMECH-IR  > 力学所知识产出(1956-2008)
Performance of a Detonation Driven Shock Tunnel
Zhao W(赵伟); Jiang ZL(姜宗林); Saito T; Lin JM(林建民); Yu HR(俞鸿儒); Takayama K; Zhao, W (reprint author), Tohoku Univ, Inst Fluid Sci, Shock Wave Res Ctr, Aoba Ku, 2-1-1 Katahira, Sendai, Miyagi 9808577, Japan.
Source PublicationShock Waves
2005
Volume14Issue:1-2Pages:53-59
ISSN0938-1287
AbstractA detonation driven shock tunnel is useful as a ground test facility for hypersonic flow research. By attaching a convergent section ahead of the primary diaphragm in the driver section, the downstream operation mode became available to generate a high-enthalpy test flow. A 100 mm diameter shock tunnel was for the first time installed in the Laboratory of High-Temperature-Gas Dynamics (LHD), Institute of Mechanics, Chinese Academy of Sciences, and after its continuous refitments, a high performance detonation driven shock tunnel was achieved to generate high-enthalpy and high-Reynolds number test flows. A new method to burst a metal diaphragm with the downstream operation mode is discussed.
Subject Area力学
DOI10.1007/s00193-004-0238-1
Indexed BySCI
Language英语
WOS IDWOS:000229628900008
WOS Research AreaMechanics
WOS SubjectMechanics
Citation statistics
Cited Times:17[WOS]   [WOS Record]     [Related Records in WOS]
Document Type期刊论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/15501
Collection力学所知识产出(1956-2008)
Corresponding AuthorZhao, W (reprint author), Tohoku Univ, Inst Fluid Sci, Shock Wave Res Ctr, Aoba Ku, 2-1-1 Katahira, Sendai, Miyagi 9808577, Japan.
Recommended Citation
GB/T 7714
Zhao W,Jiang ZL,Saito T,et al. Performance of a Detonation Driven Shock Tunnel[J]. Shock Waves,2005,14,1-2,:53-59.
APA 赵伟.,姜宗林.,Saito T.,林建民.,俞鸿儒.,...&Zhao, W .(2005).Performance of a Detonation Driven Shock Tunnel.Shock Waves,14(1-2),53-59.
MLA 赵伟,et al."Performance of a Detonation Driven Shock Tunnel".Shock Waves 14.1-2(2005):53-59.
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