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dc.contributor.authorMa, Zhuang
dc.contributor.authorLee, Shibo
dc.contributor.authorZhao, Yunlong
dc.contributor.authorZhang, Yang
dc.date.accessioned2025-04-21T10:36:08Z
dc.date.available2025-04-21T10:36:08Z
dc.date.copyright11/21/2024 12:00:00 AM
dc.date.issued2024
dc.identifier.issn0098-2202
dc.identifier.otherfe_147_04_041202.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4306529
dc.description.abstractThe primary aim of this study is to analyze the unsteady characteristics of the interaction between a reflected shock wave and a laminar boundary layer in an end-wall shock tube. Our direct numerical simulations at shock Mach numbers of Ms = 1.9, 2.5, and 3.5 using a fifth-order WENO scheme and three-step Runge–Kutta time integration method revealed inhomogeneity and anisotropy in the shock bifurcation. Surprisingly, the upper and lower bifurcated structures maintain a notably asymmetric flow during the forward propagation of the reflected shock bifurcation. The inverse flow in the bifurcation resembles a crooked earthworm structure, exhibiting high-frequency oscillations indicative of instability. However, at higher shock intensities, the earthworm transforms into a stable strip-like configuration, facilitating the entrapment of inverse flow and leading to rapid bifurcation height growth and early convergence. Additionally, isolated islands with high density, temperature, and pressure emerge in the transitional region behind the bifurcated shocks, due to variations in wave propagation speed.
dc.publisherThe American Society of Mechanical Engineers (ASME)
dc.titleNumerical Study of Bifurcation Structures in Reflected Shock-Wave/Laminar-Boundary-Layer Interaction Within an End-Wall Tube
dc.typeJournal Paper
dc.journal.volume147
dc.journal.issue4
dc.journal.titleJournal of Fluids Engineering
dc.identifier.doi10.1115/1.4066929
dc.journal.fristpage41202-1
dc.journal.lastpage41202-12
dc.page12
dc.treeJournal of Fluids Engineering:;2024:;volume( 147 ):;issue: 004
dc.contenttypeFulltext


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