放牧
发表于 2025-3-30 10:27:41
Conference proceedings 2018 and Shock Vortex Interaction Symposia. These scientific biannual meetings provide an ideal platform to expose new developments and discuss recent challenges in the field of shock wave interaction phenomena. The goal of the symposia is to offer a forum for international interaction between young and
OUTRE
发表于 2025-3-30 14:46:34
Scale Effects on the Transition of Reflected Shock Waves,over concave and convex walls of radii from 20 to 300 mm were experimentally obtained and compared with the numerical simulation based on the Navier–Stokes equations. The experimental critical transition angles varied with the radii of curved walls and strongly affected by the presence of the bounda
扩音器
发表于 2025-3-30 20:34:27
Transition Effect on Shock Wave Boundary Layer Interaction on Compressor Blade,rag or losses reduction, depending on the application. Nevertheless, in some applications, the laminar layer interaction with the shock wave may lead to a strong flow separation. The process of separation usually becomes unsteady and causes buffeting at airfoils and shock oscillations in the interna
Brain-Waves
发表于 2025-3-30 21:30:33
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CUMB
发表于 2025-3-31 02:42:39
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使成整体
发表于 2025-3-31 07:29:19
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Laconic
发表于 2025-3-31 12:10:10
Forecasting Method of Shock-Standoff Distance for Forward-Facing Cavity,ff distance, and oscillation characteristics are captured by the high-speed movie, and the dynamic pressure response is used to correlate with the acoustic characteristics of the cavity base through the transducer. By analyzing the amount of experimental and numerical results abroad, a forecasting m
exacerbate
发表于 2025-3-31 13:43:27
Shock Interactions in Continuum and Rarefied Conditions Employing a Novel Gas-Kinetic Scheme,ck interactions in partially rarefied hypersonic flows predicted employing a recently developed gas-kinetic scheme for diatomic gases with rotational degrees of freedom. The new gas-kinetic schemes will be presented along with shock/wave boundary interactions as well as Edney Type IV shock–shock int
Decline
发表于 2025-3-31 20:30:56
Ballistic Range Experiment of Shock Stand-Off Distance for Spheres in Air with Flight Speeds Betweenumerical methods, measurement of shock stand-off distance for hypersonic sphere has been conducted in the hypervelocity ballistic range of China Aerodynamic Research and Development Center. The measurement was made for spheres with diameters of 8, 10, 12 and 15 mm, flight speeds between 5.08 and 6.
Carcinogenesis
发表于 2025-4-1 00:36:18
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