2D Turbulent Flow Analysis around a 30P30N Airfoil using Adaptive Mesh Refinement on Hierarchical Cartesian Mesh

DOI Web Site Web Site 3 References
  • Shu Kembun
    連絡先著者（Corresponding author）：k-shu@g.ecc.u-tokyo.ac. jp 東京大学大学院工学系研究科航空宇宙工学専攻
  • Tamaki Yoshiharu
    東北大学大学院工学研究科航空宇宙工学専攻
  • Imamura Taro
    東京大学大学院工学系研究科航空宇宙工学専攻

Bibliographic Information

Other Title
  • Adaptive Mesh Refinementを用いた階層型直交格子による 30P30N周り流れ場の2次元乱流解析
  • Adaptive Mesh Refinement オ モチイタ カイソウガタ チョッコウ ゴウシ ニ ヨル 30P30N マワリ ナガレバ ノ 2ジゲン ランリュウ カイセキ

Search this article

Description

<p>This paper presents the accuracy improvement of CFD analysis of turbulent flow around High-Lift Devices (HLD) using Hierarchical Cartesian Mesh, which is combined with Immersed Boundary Method, Wall Function, and Adaptive Mesh Refinement (AMR). When analyzing flow around HLD under high lift condition, the flow is deflected largely and the region away from the HLD should be also resolved sufficiently. However, Hierarchical Cartesian Mesh tends to be coarse in that region. To solve this problem, AMR based on flow field variables is introduced. First, implemented AMR method is validated, and it is shown that flow features such as shock wave or wake region can be detected automatically. Then, AMR is applied to the CFD analysis of HLD using Hierarchical Cartesian Mesh. As a result, the wake region is highly resolved, and the accuracy of the analysis especially at high angle-of-attack is improved. </p>

Journal

References(3)*help

See more

Keywords

Details 詳細情報について

Report a problem

Back to top