@inproceedings{oai:jaxa.repo.nii.ac.jp:00006631,
 author = {松島, 紀佐 and 新海, 裕之 and 塩川, 将史 and 中橋, 和博 and Matsushima, Kisa and Shinkai, Hiroyuki and Shiokawa, Masashi and Nakahashi, Kazuhiro},
 book = {宇宙航空研究開発機構特別資料: 航空宇宙数値シミュレーション技術シンポジウム2003論文集, JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2003},
 month = {Mar},
 note = {In this article, it is shown that the design of a new airfoil can be performed on an ordinary Personal Computer. A software system consisting of Computational Fluid Dynamics and Graphical User Interface programs has been developed to be an aerodynamic design workbench. It is a user-friendly system for non-CFD professionals. The inverse design using the Takanashi's method can be conducted with the system as well as the analysis of the aerodynamic performance of an airfoil can be. It also provides a helpful tool for specifying appropriate target pressure distribution. The design of new concept airfoils has been performed with the system on a PC., 資料番号: AA0047427030, レポート番号: JAXA-SP-03-002},
 pages = {166--171},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {PC上で行う翼設計と性能解析},
 volume = {JAXA-SP-03-002},
 year = {2004}
}