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64303020.pdf1.89 MB
title超音速機高揚力装置形態に関する格子自動生成
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)
宇宙航空研究開発機構
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
VolumeJAXA-SP-08-009
Publication date2009-02-27
Languagejpn
eng
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
ISSN1349-113X
NCIDAA11984031
SHI-NOAA0064303020
Report NoJAXA-SP-08-009
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/15223


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