Titlebook: Shock Waves @ Marseille III; Shock Waves in Conde Raymond Brun,Lucien Z. Dumitrescu Conference proceedings 1995 Springer-Verlag Berlin Heid

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Shock Wave Impact on Porous Materialsoad, as well as allowing flow through it, and particularly the case where the matrix compressibility is somewhat lower than that of the fluid. Such materials, when placed adjacent to a rigid wall exhibit the interesting property of amplifying the reflected pressure above that that would have been ac

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On the Importance of the Basset History Term on the Particle Motion Induced by a Plane Shock Wavernal pressure gradient) on the shock wave propagation through a gas-particle mixture were evaluated by one-dimensional numerical analysis. The temporal evolution of the different forces at various locations in the low pressure section of the shock tube were evaluated for different particle response

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Experimental and Numerical Investigation of Shock Wave Attenuation in Dust-Gas Suspensionsn was conducted twice, each time using a different correlation for the dust particle drag coefficient. It was shown that when the Reynolds number is relatively high (Re > 200) the solution based on the nonstationary drag coefficient provides better agreement with experimental findings. Also studied

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Numerical Simulation of Dusty Shock Diffraction Around a 90 Degree Cornerme respectively for the gas and particle phases, the governing equations are solved based on the operator-splitting technique and predictor-corrector method. The computational predictions for pure gas flows show good agreement with the experiments of Skews and the calculations of Carofano. The numer

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Numerical Simulation of the Interaction of a Shock Wave with a Two-Phase Interface been calculated using the PLM-algorithm based on the high-resolution Riemann solver and the MacCormack scheme. The effects of Mach number (.. = 2.0 – 5.15), inital loading ratio (. = 0.1 – 4.0) and particle diameter (.. = 10 – 100 .m) on the flow field behind the incident shock wave are investigate

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