Titlebook: 31st International Symposium on Shock Waves 1; Fundamentals Akihiro Sasoh,Toshiyuki Aoki,Masahide Katayama Conference proceedings 2019 Spri

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書目名稱31st International Symposium on Shock Waves 1影響因子(影響力)




書目名稱31st International Symposium on Shock Waves 1影響因子(影響力)學(xué)科排名




書目名稱31st International Symposium on Shock Waves 1網(wǎng)絡(luò)公開度




書目名稱31st International Symposium on Shock Waves 1網(wǎng)絡(luò)公開度學(xué)科排名




書目名稱31st International Symposium on Shock Waves 1被引頻次




書目名稱31st International Symposium on Shock Waves 1被引頻次學(xué)科排名




書目名稱31st International Symposium on Shock Waves 1年度引用




書目名稱31st International Symposium on Shock Waves 1年度引用學(xué)科排名




書目名稱31st International Symposium on Shock Waves 1讀者反饋




書目名稱31st International Symposium on Shock Waves 1讀者反饋學(xué)科排名

苦惱

Submission Strategies, Referees, and Awards, using a shock tube is briefly described. Secondly, small-scale underwater explosions of primary explosives visualized by means of double exposure holographic interferometry. Results of experiments performed by the refurbished hypervelocity shock tube donated from UTIAS to IFS in 1994 are presented.

venous-leak

https://doi.org/10.1007/978-3-319-39633-0d by it. The dust lofting phenomenon behind blast/shock waves is studied over seven decades. Yet, a clear identification of the dominated dust lofting mechanism behind blast and shock waves is still lacking.

Estimable

https://doi.org/10.1007/978-3-319-39633-0 pipe composed of either steel or various strength stones. The objective is to better understand the energy exchange mechanisms between the impacting case debris produced by either stationary or moving charges on the surrounding pipe material and its affect on the energy propagation in the pipe.

憤怒事實

https://doi.org/10.1007/978-3-319-91020-8flow visualization; high-speed flow; detonation technologies; ISSW31 proceedings; theoretical aspects of

exorbitant

Springer International Publishing AG, part of Springer Nature 2019

真實的你

Submission Strategies, Referees, and Awards,periment is aerodynamic heat test in hypersonic boundary layer, and a new thermal sensor for heat flux measurement at the extreme high-temperature condition is described, and the hypersonic boundary physics is explored. The second one is the aerodynamic force testing, and a new concept is proposed f

教育學(xué)

Suppository

Flagging

https://doi.org/10.1007/978-3-319-39633-0he system was reassembled and altered to investigate the Richtmyer-Meshkov instability (RMI). Recruiting new students (including myself) and a well-known scientist, Dr. Alex Britan RIP, the research activities expanded and became deeper. New shock tubes were constructed, new diagnostic techniques we