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Numerical Investigation on Super-cooled Large Droplet Icing of Fan Rotor Blade in Jet Engine

Keisuke Isobe Masaya Suzuki Makoto Yamamoto

热科学学报(英文版)2014,Vol.23Issue(5):432-437,6.
热科学学报(英文版)2014,Vol.23Issue(5):432-437,6.DOI:10.1007/s11630-014-0726-2

Numerical Investigation on Super-cooled Large Droplet Icing of Fan Rotor Blade in Jet Engine

Numerical Investigation on Super-cooled Large Droplet Icing of Fan Rotor Blade in Jet Engine

Keisuke Isobe 1Masaya Suzuki 2Makoto Yamamoto3

作者信息

  • 1. Graduate School of Mechanical Engineering, Tokyo University of Science, 6-3-1 Niijuku, Katsushika-ku, Tokyo, 125-8585, Japan
  • 2. Aviation Program Group, Japan Aerospace Exploration Agency(JAXA), 7-44-1 Jindaiji Higashi-machi, Chofu-shi,Tokyo, 182-8522, Japan
  • 3. Department of Mechanical Engineering, Tokyo University of Science, 6-3-1 Niijuku, Katsushika-ku, Tokyo, 125-8585,Japan
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摘要

关键词

Ice Accretion/ Fan Rotor Blade/ Super-cooled Large Droplet/ Multi-physics Simulation

Key words

Ice Accretion/ Fan Rotor Blade/ Super-cooled Large Droplet/ Multi-physics Simulation

引用本文复制引用

Keisuke Isobe,Masaya Suzuki,Makoto Yamamoto..Numerical Investigation on Super-cooled Large Droplet Icing of Fan Rotor Blade in Jet Engine[J].热科学学报(英文版),2014,23(5):432-437,6.

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