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Other TitleComparison Study of High-Order Unstructured Grid Methods
Author(jpn)澤木, 悠太; 芳賀, 臣紀; 保江, かな子; 澤田, 恵介
Author(eng)Sawaki, Yuta; Haga, Takanori; Yasue, Kanako; Sawada, Keisuke
Author Affiliation(jpn)東北大学; 宇宙航空研究開発機構情報・計算工学センター(JAXA)(JEDI); 宇宙航空研究開発機構航空本部風洞技術開発センター(JAXA); 東北大学
Author Affiliation(eng)Tohoku University; JAXA's Engineering Digital Innovation Center, Japan Aerospace Exploration Agency (JAXA)(JEDI); Wind Tunnel Technology Center, Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA); Tohoku University
Issue Date2014-03-31
Japan Aerospace Exploration Agency (JAXA)
Publication title宇宙航空研究開発機構特別資料: 第45回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2013論文集
JAXA Special Publication
Start page35
End page40
Publication date2014-03-31
AbstractThe inviscid flows over ONERA-M6 wing computed by the spectral volume (SV) and discontinuous Galerkin (DG) methods are compared with that given by the conventional cell-vertex finite volume scheme using the same unstructured tetrahedral grid. In comparison, solution accuracy, and computational cost are critically examined. It is shown that both SV and DG schemes can yield highly resolved shocked flows but their computational costs are substantially higher than that of the conventional finite volume scheme. Laminar boundary layer flow and turbulent flow over 3D flat plate are also computed. In particular, v velocity in laminar flowobtained by DG scheme using hybrid cell grid agree well with the Blasius solution even with less grid resolution.
Description会議情報: 第45回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2013 (2013年7月4日-5日. タワーホール船堀), 東京
形態: カラー図版あり
Meeting Information: 45th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2013 (July 4-5, 2013. Tower Hall Funabori), Tokyo, Japan
Physical characteristics: Original contains color illustrations
Document TypeConference Paper
JAXA Category特別資料
NASA Subject CategoryFluid Mechanics and Thermodynamics
Report NoJAXA-SP-13-011

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