@inproceedings{oai:jaxa.repo.nii.ac.jp:00036953,
 author = {小濱, 泰昭 and 江上, 泰広 and Kohama, Yasuaki and Egami, Yasuhiro},
 book = {航空宇宙技術研究所特別資料, Special Publication of National Aerospace Laboratory},
 month = {Sep},
 note = {28-29 Sep. 1995 (17th). 28-29 Mar. 1996 (18th), 28-29 Sep. 1995 (17th). 28-29 Mar. 1996 (18th), すべての乱流遷移過程を、風洞中の圧力印加物体付きの偏揺れする平板上に生成した。最初に、熱線流速計と煙可視化法により、詳細な遷移過程を計測した。得られた結果から、横流れが支配的な境界層遷移中の乱流遷移は、2次不安定性に起因すると言うことができる。次に、遷移領域における流れ構造を考慮した選択的吸込システムを用いて、乱流遷移の制御を試みた。, Full turbulent transition process is created on a yawed flat plate with displacement body system in a wind tunnel. First, detailed transition process is measured by using hot wire anemometry and smoke visualization technique. From the obtained results, it can be said that turbulent transition in crossflow dominant boundary layer transition is driven by the secondary instability. Second, control of turbulent transition is tried by applying selective suction system considering flow structure in the transition region., 資料番号: AA0000867022, レポート番号: NAL SP-33},
 pages = {99--104},
 publisher = {航空宇宙技術研究所, National Aerospace Laboratory (NAL)},
 title = {横流れ不安定場の制御},
 volume = {33},
 year = {1996}
}