@inproceedings{oai:jaxa.repo.nii.ac.jp:00005603,
 author = {佐々木, 雅文 and Sasaki, Masafumi},
 book = {宇宙航空研究開発機構特別資料: 第79回風洞研究会議論文集, JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 79th Meeting},
 month = {Feb},
 note = {In this study, the aerodynamic performance of CCW (Circulation Control Wings) is investigated by two-dimensional (2D) CFD (Computational Fluid Dynamics) and the results are verified by 2D Wind-Tunnel-Test. It is found that CCW can achieve very higher lift and various lift-drag ratios at constant angle of attack (0 deg) in comparison with a conventional high-lift-device., 資料番号: AA0063897006, レポート番号: JAXA-SP-07-019},
 pages = {33--36},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {CCW空力設計技術の研究},
 volume = {JAXA-SP-07-019},
 year = {2008}
}