拥挤前 发表于 2025-3-26 23:58:09
http://reply.papertrans.cn/87/8667/866672/866672_31.pngplasma-cells 发表于 2025-3-27 03:08:09
http://reply.papertrans.cn/87/8667/866672/866672_32.pngindecipherable 发表于 2025-3-27 09:07:08
http://reply.papertrans.cn/87/8667/866672/866672_33.pngsingle 发表于 2025-3-27 10:12:44
CFD contributions to high-speed shock-related problemsp in the past, effectiveness of CFD both for design of transportation vehicles and for understanding of fluid physics is discussed. Trend of CFD for further use is then discussed based on recent applications and three key features: computer progress, spectral-like high-resolution scheme and LES and激怒某人 发表于 2025-3-27 16:14:11
http://reply.papertrans.cn/87/8667/866672/866672_35.png曲解 发表于 2025-3-27 18:37:08
Ignition delay time measurements at practical conditions using a shock tubeonditions representative of those seen in gas turbine and other engine applications. Engine conditions herein imply elevated pressures (10 atm and higher) and undiluted fuel-air mixtures. Lower temperatures (less than 1100 K) are also of interest in recent years for several reasons, including the pocartilage 发表于 2025-3-27 23:42:14
Material processing and surface reaction studies in free piston driven shock tubeamic conditions prevalent behind the reflected shock wave have been utilized to study the catalytic and non-catalytic reactions of shock heated test gases like Ar, N. or O. with different material like C. carbon, zirconia and ceria substituted zirconia. The exposed test samples are investigated usinRAG 发表于 2025-3-28 03:53:59
Molecular dynamics of shock waves in dense fluidsntially solved. Here we present a few recent findings, to show that this is not the case. There are still new physical effects to be discovered provided that the numerical technique is general enough to not rule them out a priori.组装 发表于 2025-3-28 06:31:06
http://reply.papertrans.cn/87/8667/866672/866672_39.png食料 发表于 2025-3-28 13:56:34
Shock pattern in the plume of rocket nozzles - needs for design considerationion or a Mach reflection at the nozzle centreline. Especially for rocket propulsion, other nozzle types besides the ideal nozzles are often used, including simple conical, thrust-optimized or parabolic contoured nozzles. Depending on the contour type, another shock structure may appear: the so-calle