@inproceedings{oai:jaxa.repo.nii.ac.jp:00004274,
 author = {高田, 晃輔 and 高木, 正平 and 平田, 裕 and 坂上, 昇史 and Takada, Kosuke and Takagi, Shyohei and Hirata, Yutaka and Sakaue, Shyoji},
 book = {宇宙航空研究開発機構特別資料, JAXA Special Publication: Proceedings of 44th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2012},
 month = {Mar},
 note = {第44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2012 (2012年7月5日-6日. 富山国際会議場大手町フォーラム), 富山市, 富山県, 44th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2012 (July 5-6, 2012. Toyama International Conference Center), Toyama Japan, The present paper deals with instability and transition of 3-D boundary layer developing on a yawed circular cylinder with a sweepback of 60 degrees at Mach 2 in the supersonic wind tunnel of Muroran Institute of Technology. Visualized surface flow presents many striations regularly aligned almost to inviscid streamline, while hot-wire survey shows time-dependent broad-band disturbances, both of which originate from the so called cross-flow instability. It is found that comparison of experiments and stability analyses shows good agreement. The effect of condensation in the main flow on static pressure on a 5-degree semi-vertex cone model is discussed., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0061958034, レポート番号: JAXA-SP-12-010},
 pages = {203--206},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {超音速三次元境界層の進行波モードの検出},
 volume = {JAXA-SP-12-010},
 year = {2013}
}