@inproceedings{oai:jaxa.repo.nii.ac.jp:00038084,
 author = {跡部, 隆 and Atobe, Takashi},
 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 = {The effect of accuracy of boundary layer calculations on the prediction of laminar-turbulent transition of boundary layer is examined by comparing the two scheme of boundary layer calculations, using a similarity equation and a Navier-Stokes code. The flow field is a boundary layer around an NACA0015 wing model. The Orr-Sommerfeld equations are used for the local stability analysis and the N factor of the e(sup N) method is used for a criterion. From the present study a slight difference of velocity profiles causes a significant difference of an end result., 資料番号: AA0032819048, レポート番号: NAL SP-53},
 pages = {279--284},
 publisher = {航空宇宙技術研究所, National Aerospace Laboratory (NAL)},
 title = {境界層遷移予測に対する速度分布計算精度の影響},
 volume = {53},
 year = {2002}
}