蚊帐
发表于 2025-3-28 14:50:30
Hypersonic Shock Wave Boundary Layer Interaction Studies on a Flat Plate at Elevated Surface Temper the transition process was completed in the separated shear layer, leading to a fully turbulent reattachment on the flap. The experimental effort is complemented by Reynolds-Averaged Navier–Stokes (RANS) computations providing insights into fundamental trends. The 2D simulations underpredict the si
重叠
发表于 2025-3-28 21:42:57
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疯狂
发表于 2025-3-29 01:59:39
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infatuation
发表于 2025-3-29 04:08:54
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Compassionate
发表于 2025-3-29 08:04:32
978-3-030-10329-3Springer International Publishing AG, part of Springer Nature 2018
Cytokines
发表于 2025-3-29 14:07:46
Overexpanded Jet Flow Type of Symmetry Influence on the Differential Characteristics of Flowfield irning flow parameters. Analytical results can be applied to avoid jet flow instability and self-oscillation effects at rocket launch, to improve launch safety and to suppress shock wave-induced noise harmful to environment and personnel.
惊奇
发表于 2025-3-29 17:30:15
Oblique Shock Reflection over a Membrane,to be reflected off some solid hard material. In this case, the deformation of the reflection surface is negligible even if the pressure rise is high, and the boundary condition can be easily assigned.
键琴
发表于 2025-3-29 21:18:54
Triple-Point Singularity and the Neumann Paradox of Mach Reflection, in polar coordinates, with special attention on the cause of the Neumann paradox. It gives a centered fan-like flow from the triple point in widening the slip flow region. Angles and curvatures of the reflected (.) and Mach stem (.) shock lines given in the solution are consistent with existing experiment data.
到婚嫁年龄
发表于 2025-3-30 00:19:24
Experimental Investigation of Mist Injection at the Stagnation Point of a Blunt Body in Hypersonicconfigurations are preferred as forebody to minimize aerodynamic heating. Though these configurations reduce heat transfer to some extent, they are not alone sufficient to withstand the harsh conditions existing during re-entry.
Ejaculate
发表于 2025-3-30 04:37:43
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