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Titlebook: Experimental Methods of Shock Wave Research; Ozer Igra,Friedrich Seiler Book 2016 Springer International Publishing Switzerland 2016 Exper

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發(fā)表于 2025-3-21 16:05:12 | 只看該作者 |倒序?yàn)g覽 |閱讀模式
書(shū)目名稱Experimental Methods of Shock Wave Research
編輯Ozer Igra,Friedrich Seiler
視頻videohttp://file.papertrans.cn/319/318879/318879.mp4
概述Well structured encyclopedic book.Presents a state-of the art overview on Experimental methods of Shock Wave Research.Vol. 9 of the Shock Waves Science and Technology Reference Library.Includes supple
叢書(shū)名稱Shock Wave Science and Technology Reference Library
圖書(shū)封面Titlebook: Experimental Methods of Shock Wave Research; Ozer Igra,Friedrich Seiler Book 2016 Springer International Publishing Switzerland 2016 Exper
描述.This comprehensive and carefully edited volume presents a variety of experimental methods used in Shock Waves research. In 14 self contained chapters this 9.th. volume of the “Shock Wave Science and Technology Reference Library” presents the experimental methods used in Shock Tubes, Shock Tunnels and Expansion Tubes facilities. Also described is?their set-up and operation. The uses of an arc heated wind tunnel and a gun tunnel are also contained in this volume. Whenever possible, in addition to the technical description some typical scientific results obtained using such facilities are described. Additionally, this authoritative book includes techniques for measuring physical properties of blast waves and laser generated shock waves. Information about active shock wave laboratories at different locations around the world that are not described in the chapters herein is given in the Appendix, making this book useful for every researcher involved in shock/blast wave phenomena..
出版日期Book 2016
關(guān)鍵詞Experimental Methods of Shock Wave Research; Experimental Shock Waves Research; Shock Waves; Shock Wave
版次1
doihttps://doi.org/10.1007/978-3-319-23745-9
isbn_softcover978-3-319-36776-7
isbn_ebook978-3-319-23745-9
copyrightSpringer International Publishing Switzerland 2016
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發(fā)表于 2025-3-22 00:11:51 | 只看該作者
Shock Wave Experiments in a High-Temperature Gas Flowc-heated wind tunnel is one of these facilities and features long operational time; thus the arc-heated wind tunnel has been used mainly for the development and evaluation of a thermal protection system for space transportation systems. Thus generated plasma flows can be employed for the experiments
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The Aachen Shock Tunnel TH2 with Dual Driver Mode Operationitions. Their performance range mainly depends on their driver technology which can be distinguished between conventional driver, employing pre-compressed gas, combustion and detonation driver and free piston driver. In principle, the highest performance in terms of nozzle reservoir pressure and tem
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發(fā)表于 2025-3-23 03:55:02 | 只看該作者
Shock Tunnels and Hypersonic Research in IISc, Bangalorededicated centre for the research, among other domains of fluid dynamics, on the shock dominated phenomena. More often than not, the focus of the research is on the flow phenomena at high enthalpies, which are addressed using the impulse facilities—shock tubes and tunnels. Ever since its inception a
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發(fā)表于 2025-3-23 07:56:02 | 只看該作者
Gun TunnelsGun tunnels produce low enthalpy hypersonic flows with durations of several tens of milliseconds. For a capital investment similar to that of a comparably-sized, regular shock tunnel, gun tunnels offer at least an order of magnitude longer flow duration. This makes gun tunnels an attractive option f
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