Titlebook: Shock Dynamics; Zhaoyuan Han,Xiezhen Yin Book 1993 Springer Science+Business Media Dordrecht 1993 Navier-Stokes equation.dynamics.flows.sh

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Refractions of Shock Waves at Interface Between Different Media and Interaction Between Shockstmosphere, shock-boundary layer interaction on transonic airfoils, blast wave reflection and refraction on the water surface, shock interaction with flame fronts, and shock propagation through a gas- liquid stratified system in nuclear reactors.

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Book 1993 field of Fluid Mechanics, Department of Modern Mechanics, University of Science and Technology of China for seven times. In the spring semester 1989, during his visit to the United States, the first author taught this course to the graduate students of Department of Mathemat­ ics, University of Col

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978-90-481-4159-3Springer Science+Business Media Dordrecht 1993

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Shock Dynamics978-94-017-2995-6Series ISSN 0926-5112 Series E-ISSN 2215-0056

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Introduction One-Dimensional Unsteady GasdynamicsAs a basis, this chapter introduces one-dimensional, unsteady, continuous flow of gasdynamics, in which the behaviour, concepts and relations of small amplitude wave (sound wave) and large amplitude wave are discussed.

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Relation Between , and , for a Uniform Quiescent Gas Ahead of a Shock WaveIn this chapter, we will explain the basis of shock dynamics—CCW rela­tion. So- called CCW relation is that Chester(1954), Chisnell(1957), and Whitham (1958) obtained the same relation between shock Mach number . and cross-sectional area . in a tube for a uniform quiescent gas ahead of a shock by using three different methods.

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