@inproceedings{oai:jaxa.repo.nii.ac.jp:00005422,
 author = {永田, 靖典 and 雷, 忠 and Nagata, Yasunori and Lei, Zhong},
 book = {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, JAXA Special Publication: Proceedings fo 40th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2008},
 month = {Feb},
 note = {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, An 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., 形態: カラー図版あり, 資料番号: AA0064303020, レポート番号: JAXA-SP-08-009},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {超音速機高揚力装置形態に関する格子自動生成},
 volume = {JAXA-SP-08-009},
 year = {2009}
}