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作 者:Taiki Matsuura Masaya Suzuki Makoto Yamamoto Shinichiro Shishido Takeshi Murooka Hiroshi Miyagawa
机构地区:[1]Graduate School of Mechanical Engineering, Tokyo University of Science 1-14-6, Kudankita, Chiyoda-ku [2]Department of Mechanical Engineering, Tokyo University of Science 1-14-6, Kudankita, Chiyoda-ku [3]Research and Engineering Division, IHI Corporation 229, Tonogaya, Mizuho-cho, Nishitama-gun
出 处:《Journal of Thermal Science》2012年第4期322-326,共5页热科学学报(英文版)
摘 要:Ice accretion is the phenomenon that super-cooled water droplets impinge and accrete on a body. It is well known that ice accretion on blades and airfoils leads to performance degradation and severe accidents. For this reason, experimental investigations have been carried out using flight tests or icing tunnels. However, it is too expensive, dangerous, and difficult to set actual icing conditions. Hence, computational fluid dynamics is useful to predict ice accretion. A rotor blade is one of jet engine components where ice accretes. Therefore, the authors focus on the ice accretion on a rotor blade in this study. Three-dimensional icing phenomena on the rotor blade of a commercial axial blower are computed here, and ice accretion on the rotor blade is numerically investigated.
关 键 词:ICING Computational Fluid Dynamics Euler-Lagrangian Coupling Rotor Blade Axial Blower
分 类 号:TH453[机械工程—机械制造及自动化]
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