Results 1 to 10 of about 116,621 (216)
Effects of a nonadiabatic wall on supersonic shock/boundary-layer interactions [PDF]
Physical Review Fluids, 2018 Direct numerical simulations are employed to investigate a shock wave impinging on a turbulent boundary layer at free-stream Mach number M=2.28 with different wall thermal conditions, including adiabatic, cooled, and heated, for a wide range of ...
Bernardini, M. +2 more
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Research Progress of Microjet Control of Shock Wave/Boundary Layer Interactions in Supersonic Flow Field [PDF]
Hangkong bingqi, 2022 The phenomenon of shock wave/boundary layer interaction is inevitable in the supersonic flow field. The existence of this phenomenon will have a series of adverse effects on the inner and outer flow fields of the supersonic vehicle.
Xu Hao, Du Zhaobo, Zhong Xiangyu, Huang Wei
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气体物理, 2023 In order to explore the effect of entropy layer on swept shock/turbulent boundary layer interaction, numerical simulation was applied to study a fin/blunt plate physical model.
Xian-kai LI +6 more
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Fluids, 2022 Although it is understood that surface roughness can impact boundary layer physics in high-speed flows, there has been little research aimed at understanding the potential impact of surface roughness on high-speed shock-wave/boundary-layer interactions ...
Matt Garcia +7 more
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Aerospace, 2023 Compression corner shock wave/boundary layer interaction (SWBLI) is a typical shock wave/boundary layer interaction (SWBLI) problem in supersonic/hypersonic flows. In previous studies, the separation flow is usually caused by a single shock wave. However,
Bo Yang +5 more
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Unsteady Motion of Shock Wave for a Supersonic Compression Ramp Flow Based on Large Eddy Simulation
Frontiers in Energy Research, 2022 A large eddy simulation (LES) is conducted to investigate shock wave/turbulent boundary layer interaction in a 24° compression ramp at a high inlet Mach number of Ma=2.9.
Xing Huang +3 more
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Numerical Investigation of Mach 2.5 Axisymmetric Turbulent Shock Wave Boundary Layer Interactions
Aerospace, 2023 Shock wave boundary layer interactions are common to both supersonic and hypersonic inlet flows. Wall-resolved implicit large-eddy simulations of a canonical Mach 2.5 axisymmetric shock wave boundary layer interaction experiment at Glenn Research Center ...
John-Paul Mosele +2 more
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Shock boundary layer interactions in dense gases [PDF]
PAMM, 2004 AbstractThe concept of triple deck theory is applied to study laminar interacting boundary layers of dense gases in external purely supersonic flow. An impinging shock is generated at distances which are large compared to the upper deck thickness. As predicted by weakly nonlinear theory such a discontinuity may disintegrate into a sonic shock and an ...
Alfred Kluwick, Marcus Wrabel
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TASK Quarterly, 2015 The shock wave boundary layer interaction on the suction side of a transonic compressor blade is one of the main objectives of the TFAST project (Transition Location Effect on Shock Wave Boundary Layer Interaction).
MICHAŁ PIOTROWICZ +2 more
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Oblique Shock Wave/Axisymmetric Boundary-Layer Interactions
气体物理, 2023 Menter's SST two-equation turbulence model was used to simulate the interaction between oblique shock wave and axisymmetric boundary layer in a supersonic Mach 3 flow, and the results were analyzed qualitatively and quantitatively.
Liu-qing YANG, Qin LI, Yan-cheng YOU
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