混合 发表于 2025-3-23 10:35:44
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 acBudget 发表于 2025-3-23 16:40:39
http://reply.papertrans.cn/87/8667/866677/866677_12.pnganimated 发表于 2025-3-23 19:54:29
http://reply.papertrans.cn/87/8667/866677/866677_13.pngConscientious 发表于 2025-3-24 00:19:06
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 responsedefenses 发表于 2025-3-24 06:16:58
http://reply.papertrans.cn/87/8667/866677/866677_15.pngadipose-tissue 发表于 2025-3-24 07:03:53
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 studiedAllure 发表于 2025-3-24 13:48:39
http://reply.papertrans.cn/87/8667/866677/866677_17.pngDEMN 发表于 2025-3-24 16:15:31
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吹牛需要艺术 发表于 2025-3-24 20:03:28
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不怕任性 发表于 2025-3-24 23:09:23
http://reply.papertrans.cn/87/8667/866677/866677_20.png