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Changes in the type of the shock-wave structure in high-velocity flows
Authors:G A Tarnavsky
Institution:(1) Institute of Theoretical and Applied Mechanics, Siberian Division, Russian Academy of Sciences, 630090 Novosibirsk
Abstract:Physical aspects of nonuniqueness of shock-wave structures in supersonic and hypersonic flows are considered. Thermodynamic conditions determining the dual solution domains are analyzed, and the boundaries of the transition from Mach to regular reflection are examined.Translated from Prikladnaya Mekhanika i Tekhnicheskaya Fizika, Vol. 46, No. 2, pp. 23–32, March–April, 2005.
Keywords:mathematical simulation  gas dynamics  solution nonuniqueness  shock waves  Mach and regular reflection
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