No AccessTechnical NoteAnalytical Solutions of Shock Structure Thickness and Asymmetry in Navier–Stokes/Fourier FrameworkR. S. MyongR. S. MyongDepartment of Aerospace and System Engineering and Research Center for Aircraft Parts Technology, Gyeongsang National University, Gyeongnam 660-701, Republic of KoreaPublished Online:22 Apr 2014https://doi.org/10.2514/1.J052583SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations About References [1] Becker R., "Stosswelle und Detonation," Zeitschrift für Physik, Vol. 8, No. 1, 1922, pp. 321–362. CrossrefGoogle Scholar[2] Taylor G. I. and Maccoll J. W., "Mechanics of Compressible Fluids," Aerodynamics Theory, Durand W. F. (ed.), Vol. 3, Springer, Berlin, 1934. Google Scholar[3] Morduchow M. and Libby P. A., "On a Complete Solution of the One-Dimensional Flow Equations of a Viscous, Heat-Conducting, Compressible Gas," Journal of the Aeronautical Sciences, Vol. 16, No. 11, 1949, pp. 674–684, 704. 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