1993
DOI: 10.1007/bf01051192
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Reflection of a blast-profile shock wave from the end wall of a shock tube

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Cited by 6 publications
(4 citation statements)
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“…The Mach number of the shock wave also increased in the shock tube when the pressure ratio across the diaphragm was increased. After the incident shock reached the end wall of the shock tube, the reflected shock traveled back into the oncoming gases because it is stopped by the end wall of the shock tube (9, 10). …”
Section: Complex Shock Waves Inside Shock Tubementioning
confidence: 99%
“…The Mach number of the shock wave also increased in the shock tube when the pressure ratio across the diaphragm was increased. After the incident shock reached the end wall of the shock tube, the reflected shock traveled back into the oncoming gases because it is stopped by the end wall of the shock tube (9, 10). …”
Section: Complex Shock Waves Inside Shock Tubementioning
confidence: 99%
“…Some of these results are also used in the present study to demonstrate some of the new points that are raised in the discussion section. Further information on this technique of generating blast-like pressure profiles can be found in Britan et al (1993).…”
Section: Short Driver Shock Tubementioning
confidence: 99%
“…For physical simulation of the high-explosive blast impact on a target (protected) object in Russia [1][2][3][4] and abroad [5][6][7][8][9][10][11], shock tubes are traditionally used. The advantages of this method of physical simulation over full-scale field tests are lower cost and easier reproducibility of the experiment, as well as its higher safety.…”
Section: Introductionmentioning
confidence: 99%
“…The problems of constructing shock tubes with a given pressure profile of the resulting waves were previously solved numerically and analytically [3,12,13]. The increased attention paid nowadays to testing various means of explosion protection makes it necessary to consider this issue in more detail.…”
Section: Introductionmentioning
confidence: 99%