JAXA Repository / AIREX 未来へ続く、宙(そら)への英知
61958011.pdf1.32 MB
title任意多面体非構造圧縮性ソルバーLS-FLOWにおける重合格子法開発
Other TitleDevelopment of Overset CFD Technology in Unstructured, Compressible Flow Solver for Arbitrary Polyhedral Meshes, LS-FLOW
Author(jpn)青野, 淳也; 葛生, 和人
Author(eng)Aono, Junya; Kuzuu, Kazuto
Author Affiliation(jpn)株式会社計算力学研究センター; 宇宙航空研究開発機構情報・計算工学センター(JAXA)(JEDIC)
Author Affiliation(eng)Research Center of Computational Mechanics, Inc.; JAXA's Engineering Digital Innovation Center, Japan Aerospace Exploration Agency (JAXA)(JEDIC)
Issue Date2013-03-29
Publisher宇宙航空研究開発機構(JAXA)
Japan Aerospace Exploration Agency (JAXA)
Publication title宇宙航空研究開発機構特別資料
JAXA Special Publication: Proceedings of 44th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2012
VolumeJAXA-SP-12-010
Start page61
End page66
Publication date2013-03-29
Languagejpn
eng
AbstractThe overset grid approach provides a very powerful means of handling complex geometries in computational fluid dynamics. The overset grid approach has many practical benefits for unsteady moving grid simulation or rudder angle. Therefore an overset unstructured grid method was newly developed for an arbitrary polyhedral compressible flow solver, LS-FLOW. We set the IBlank for visualization and post-processing. In order to test the validity of the suggested methods, a numerical simulation was carried out on the NACA0012 airfoil.And our results are compared with experimental data and other CFD results. Furthermore, in order to evaluate the validity of this method, we also simulated the flow around a reusable sounding rocket under research at JAXA//ISAS. The result of the overset grid method corresponds with the result of the single grid method in the NACA0012 airfoil and the reusable sounding rocket. The good coincidence validates our newly deve""" loped overset grid method, and intend to use LS-FLOW as a design tool.
Description会議情報: 第44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2012 (2012年7月5日-6日. 富山国際会議場大手町フォーラム), 富山市, 富山県
形態: カラー図版あり
Meeting Information: 44th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2012 (July 5-6, 2012. Toyama International Conference Center), Toyama Japan
Physical characteristics: Original contains color illustrations
Document TypeConference Paper
JAXA Category特別資料
ISSN1349-113X
NCIDAA11984031
SHI-NOAA0061958011
Report NoJAXA-SP-12-010
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/13875


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