In the present study, we investigate the two-dimensional laminar flow through a one-sided constriction of a plane channel with a ratio of h : H=1:4 ( where h is the step height and H is the channel height). The computational approach employed is based on a mixed implicit/explicit time discretization scheme together with a highly accurate spatial discretization using a P-N - PN-2 spectral-element method. It is well known that this so-called forward-facing step (FFS) flow exhibits a singularity in the pressure and the velocity derivatives at the corner point. We account for this singularity by a geometric mesh refinement strategy that was proposed in a hp-FEM context. A detailed numerical study of the FFS flow reveals that length and height of the recirculation zone in front of the step are almost constant for creeping flow. In the limit of high Reynolds numbers the length and height of the recirculation zone increase proportional to Re-0.6 and Re-0.2, respectively.
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Moscow MV Lomonosov State Univ, Res Inst Mech, 1 Michurinsky Ave, Moscow 119192, RussiaMoscow MV Lomonosov State Univ, Res Inst Mech, 1 Michurinsky Ave, Moscow 119192, Russia
Simonenko, Mikhail
Zubkov, Alexander
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Moscow MV Lomonosov State Univ, Res Inst Mech, 1 Michurinsky Ave, Moscow 119192, RussiaMoscow MV Lomonosov State Univ, Res Inst Mech, 1 Michurinsky Ave, Moscow 119192, Russia
Zubkov, Alexander
Kuzmin, Alexander
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St Petersburg State Univ, 28 Univ Ave, St Petersburg 198504, RussiaMoscow MV Lomonosov State Univ, Res Inst Mech, 1 Michurinsky Ave, Moscow 119192, Russia
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China Aerodynam Res & Dev Ctr, Hyperveloc Aerodynam Inst, Mianyang 621000, Peoples R ChinaChina Aerodynam Res & Dev Ctr, Hyperveloc Aerodynam Inst, Mianyang 621000, Peoples R China
Zhang, Qing-Hu
Zhu, Tao
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China Aerodynam Res & Dev Ctr, Hyperveloc Aerodynam Inst, Mianyang 621000, Peoples R ChinaChina Aerodynam Res & Dev Ctr, Hyperveloc Aerodynam Inst, Mianyang 621000, Peoples R China
Zhu, Tao
Yi, Shihe
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Natl Univ Def Technol, Coll Aerosp Sci & Technol, Changsha 410073, Hunan, Peoples R ChinaChina Aerodynam Res & Dev Ctr, Hyperveloc Aerodynam Inst, Mianyang 621000, Peoples R China
Yi, Shihe
Wu, Anping
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China Aerodynam Res & Dev Ctr, Hyperveloc Aerodynam Inst, Mianyang 621000, Peoples R ChinaChina Aerodynam Res & Dev Ctr, Hyperveloc Aerodynam Inst, Mianyang 621000, Peoples R China
机构:
Hypervelocity Aerodynamics Institute of China Aerodynamics Research and Development CenterHypervelocity Aerodynamics Institute of China Aerodynamics Research and Development Center
张庆虎
朱涛
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Hypervelocity Aerodynamics Institute of China Aerodynamics Research and Development CenterHypervelocity Aerodynamics Institute of China Aerodynamics Research and Development Center
朱涛
易仕和
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College of Aerospace Science and Technology, National University of Defense TechnologyHypervelocity Aerodynamics Institute of China Aerodynamics Research and Development Center
易仕和
吴岸平
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Hypervelocity Aerodynamics Institute of China Aerodynamics Research and Development CenterHypervelocity Aerodynamics Institute of China Aerodynamics Research and Development Center
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Univ London Imperial Coll Sci Technol & Med, Dept Aeronaut, London SW7 2AZ, EnglandUniv London Imperial Coll Sci Technol & Med, Dept Aeronaut, London SW7 2AZ, England
Pearson, D. S.
Goulart, P. J.
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Univ London Imperial Coll Sci Technol & Med, Dept Aeronaut, London SW7 2AZ, England
ETH, Automat Control Lab, CH-8092 Zurich, SwitzerlandUniv London Imperial Coll Sci Technol & Med, Dept Aeronaut, London SW7 2AZ, England