JAXA Repository / AIREX 未来へ続く、宙(そら)への英知
64303020.pdf1.89 MB
Other TitleAutomatic grid generation for a supersonic transport configuration with high-lift devices
Author(jpn)永田, 靖典; 雷, 忠
Author(eng)Nagata, Yasunori; Lei, Zhong
Author Affiliation(jpn)菱友システムズ; 宇宙航空研究開発機構航空プログラムグループ
Author Affiliation(eng)Ryoyu Systems; Aviation Program Group, Japan Aerospace Exploration Agency (APG)(JAXA)
Issue Date2009-02-27
PublisherJapan Aerospace Exploration Agency (JAXA)
Publication titleJAXA special publication: Proceedings fo 40th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2008
宇宙航空研究開発機構特別資料: 第40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2008論文集
Publication date2009-02-27
AbstractAn automatic grid tool for a supersonic transport configuration with leading- and trailing-edge flaps was developed. It employed the commercial software Gridgen to modify the shape and grid for different combination of flap deflection angles. With the automatic tool, time cost for shape modification and grid generation is dramatically reduced. In this paper, the automatic process of shape modification and grid generation are described, and examples of the generated grid and computational result are presented.
Description形態: カラー図版あり
会議: 第40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2008. 会期: 2008年6月12日-6月13日. 会場: 東北大学片平キャンパス
KeywordsHigh-lift device, Automatic Grid Generation, CFD
Document TypeTechnical Report
JAXA Category特別資料
Report NoJAXA-SP-08-009

Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.