@inproceedings{oai:jaxa.repo.nii.ac.jp:00005470,
 author = {徳川, 直子 and 郭, 東潤 and 吉田, 憲司 and Tokugawa, Naoko and Kwak, Dong-Youn and Yoshida, Kenji},
 book = {宇宙航空研究開発機構特別資料: 境界層遷移の解明と制御研究会講演論文集（第41回・第42回）, JAXA Special Publication: Proceedings of the 41st and 42nd JAXA Workshops on Investigation and Control of Boundar-Layer Transition},
 month = {Feb},
 note = {第41回「境界層遷移の解明と制御」研究会（2007年10月4日-10月5日）, The experimental validation of Natural Laminar Flow wing designed with our original CFD-based inverse design method is carried out by the flight test of an unmanned and scaled supersonic experimental airplane. To add the reliability to the validation of Natural Laminar Flow wing concept, the data analysis method and numerical prediction method is investigated and improved., 形態: カラー図版あり, 資料番号: AA0064237012, レポート番号: JAXA-SP-08-006},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {小型超音速ロケット実験機の遷移判定},
 volume = {JAXA-SP-08-006},
 year = {2009}
}