@inproceedings{oai:jaxa.repo.nii.ac.jp:00038082,
 author = {野村, 聡幸 and 黒田, 文武 and Nomura, Toshiyuki and Kuroda, Fumitake},
 book = {航空宇宙技術研究所特別資料: 航空宇宙数値シミュレーション技術シンポジウム2001論文集, Special Publication of National Aerospace Laboratory: Proceedings of Aerospace Numerical Simulation Symposium 2001},
 month = {Jan},
 note = {In the experiments conducted at FHI, boundary-layer transition was observed on the outer wing of the SST half model. In many cases, boundary-layer transition on a swept wing has been caused by the growth of crossflow disturbances. Then, the spatial growth of crossflow disturbances on the outer wing is investigated using the prediction system of boundary-layer transition. The results show their growth is too small to cause transition. It is fairly possible that the transition observed in the experiments was caused by TS waves., 資料番号: AA0032819046, レポート番号: NAL SP-53},
 pages = {267--272},
 publisher = {航空宇宙技術研究所, National Aerospace Laboratory (NAL)},
 title = {SST外翼上での横流れ擾乱の空間増幅},
 volume = {53},
 year = {2002}
}