@inproceedings{oai:jaxa.repo.nii.ac.jp:00006562,
 author = {稲澤, 歩 and 伊澤, 精一郎 and 福西, 祐 and Inasawa, Ayumu and Izawa, Seiichiro and Fukunishi, Yu},
 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33回・第34回, JAXA Special Publication: Proceedings of the 33rd and 34th JAXA Workshops on Investigation and Control of Boundary-Layer Transition},
 month = {Jan},
 note = {Development of point source disturbance in the three-dimensional boundary layer of yawed circular cylinders is studied using Direct Numerical Simulation (DNS). Using a 2D FFT technique, the waves are separated into two instability modes. One is the streamline-curvature instability and the other is the cross-flow instability as predicted theoretically. It is shown that the T-S wave type instability appears when the frequency of excited disturbance is high, while the cross-flow instability becomes dominant when the frequency is low., 資料番号: AA0047776008, レポート番号: JAXA-SP-04-002},
 pages = {25--28},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {後退円柱における不安定波の数値シミュレーション},
 volume = {JAXA-SP-04-002},
 year = {2005}
}