caa a22 4500 467954453 CHVBK 20180405193745.0 cr unu---uuuuu 170328e20050301xx s 000 0 eng 10.1007/PL00021893 doi (NATIONALLICENCE)springer-10.1007/PL00021893 (NATIONALLICENCE)springer-10.1007/s10808-005-0026-4 Tarnavsky G. Institute of Theoretical and Applied Mechanics, Siberian Division, Russian Academy of Sciences, 630090, Novosibirsk aut Changes in the type of the shock-wave structure in high-velocity flows [Elektronische Daten] [G. Tarnavsky] 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. Springer Science+Business Media, Inc., 2005 mathematical simulation nationallicence gas dynamics nationallicence solution nonuniqueness nationallicence shock waves nationallicence Mach and regular reflection nationallicence Journal of Applied Mechanics and Technical Physics Kluwer Academic Publishers-Consultants Bureau 46/2(2005-03-01), 168-175 0021-8944 46:2<168 2005 46 10808 https://doi.org/10.1007/PL00021893 text/html Onlinezugriff via DOI 1 research-article jats NATIONALLICENCE 856 40 https://doi.org/10.1007/PL00021893 text/html Onlinezugriff via DOI NATIONALLICENCE 100 1- Tarnavsky G. Institute of Theoretical and Applied Mechanics, Siberian Division, Russian Academy of Sciences, 630090, Novosibirsk aut NATIONALLICENCE 773 0- Journal of Applied Mechanics and Technical Physics Kluwer Academic Publishers-Consultants Bureau 46/2(2005-03-01), 168-175 0021-8944 46:2<168 2005 46 10808 NATIONALLICENCE 856 40 https://doi.org/10.1007/s10808-005-0026-4 text/html Onlinezugriff via DOI Metadata rights reserved Springer special CC-BY-NC licence nationallicence BK010053 XK010053 XK010000 NATIONALLICENCE NATIONALLICENCE NL-springer NATIONALLICENCE NATIONALLICENCE NL-springer