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Published in 2021 at "Acta Astronautica"
DOI: 10.1016/j.actaastro.2021.08.050
Abstract: Abstract Shock wave–boundary layer interaction (SWBLI) is one of the most prevalent challenges in the field of fluid mechanics. Excessive interaction may lead to strong flow separation, which is an important factor causing the deterioration… read more here.
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Published in 2017 at "Journal of Fluid Mechanics"
DOI: 10.1017/jfm.2017.610
Abstract: We study so-called wave boundary layers (BLs) arising in a stably stratified fluid at large times. The BL is a narrow domain near the surface and/or bottom of the fluid; with increasing time, gradients of… read more here.
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Published in 2025 at "Journal of Fluid Mechanics"
DOI: 10.1017/jfm.2025.10597
Abstract: Abstract The flow instabilities in shock-wave–boundary-layer interactions at Mach 6 are comprehensively investigated through compression corner and incident shock cases. The boundary of global stability and the characteristics of globally unstable modes are determined by… read more here.
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Published in 2023 at "AIP Advances"
DOI: 10.1063/5.0149490
Abstract: The shock wave/boundary layer interaction phenomenon is harmful to the performance improvement of the hypersonic vehicle, and the microjet flow control scheme was introduced to minimize the total volume of the separation bubble and maximize… read more here.
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Published in 2025 at "Physics of Fluids"
DOI: 10.1063/5.0304202
Abstract: Shock-wave/boundary-layer interactions (SWBLIs) have been a hot and long-standing issue in the aerospace field. In strong interactions, the boundary layer separates under the influence of adverse pressure gradients, and the interaction length is a key… read more here.
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Published in 2017 at "Oceanology"
DOI: 10.1134/s0001437017020175
Abstract: The paper examines so-called wave boundary layers arising in a bounded stratified fluid for large times. Each the layer is a narrow domain in the vicinity of the fluid surface and/or bottom characterized by sharp,… read more here.
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Published in 2018 at "Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering"
DOI: 10.1177/0954410016687142
Abstract: Shock wave and tip leakage are important flow features at small length scales. These flow phenomena and their interactions play important roles in the performance of modern transonic fans and compressors. In most numerical predictions… read more here.
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Published in 2025 at "Journal of Spacecraft and Rockets"
DOI: 10.2514/1.a36312
Abstract: Hypersonic flow over axisymmetric bodies with four evenly spaced fins was investigated computationally. The test conditions encompassed a freestream Mach number of 5.9 and Reynolds numbers based on body length of [Formula: see text] and… read more here.
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Published in 2017 at "AIAA Journal"
DOI: 10.2514/1.j055575
Abstract: This study examines establishment times of shock-wave/boundary-layer interactions across a range of interaction types and intermittent facilities. Successful design of a test article for a short-du... read more here.
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Published in 2020 at "AIAA Journal"
DOI: 10.2514/1.j059184
Abstract: The three-dimensional (3-D) shock-wave/boundary-layer interaction (SBLI) between a fin-generated shock and a turbulent boundary layer is examined using plenoptic particle image velocimetry (PIV): a... read more here.