Abstract
The random choice method (RCM) was used to numerically solve shock propagation in a Laval nozzle and a Ludwieg tube. In quasi-random sampling procedure, van der Corput method was used. According to each specified incident shock Mach number and nozzle area ratio, the RCM analysis predicts five unique possible wave patterns. The starting process of the Ludwieg tube was also numerically analyzed by using the RCM.
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