@inproceedings{oai:jaxa.repo.nii.ac.jp:00037674,
 author = {Lin, R.-S. and Reed, H.L.},
 book = {航空宇宙技術研究所特別資料, Special Publication of National Aerospace Laboratory},
 month = {Nov},
 note = {航空宇宙技術研究所 24-25 Sep. 1991 (9th). 16-18 Mar. 1992 (10th) 東京 日本, National Aerospace Laboratory 24-25 Sep. 1991 (9th). 16-18 Mar. 1992 (10th) Tokyo Japan, 後退翼上の境界層の安定計算において、壁面と流線の曲率を考慮に入れた場合の効果を調べた。まず、線形攪乱方程式を物体面に沿う固定した曲線座標系で記述する。次に、この定式化において、主として流線曲率効果に貢献する非平行流効果項を残してそれらを局所的な差分値で近似する。凸面壁の曲率は流れの安定性を強める一方、流線の曲率は不安定化に向けて働らく。, The effect of including wall and streamline curvature terms in swept-wing boundary-layer stability calculations is studied. The linear disturbance equations are cast on a fixed, body-intrinsic, curvilinear coordinate system. Those nonparallel terms which contribute mainly to the streamline-curvature effect are retained in this formulation and approximated by their local finite-difference values. Convex wall curvature has a stabilizing effect, while streamline curvature is destabilizing., 資料番号: AA0004167012, レポート番号: NAL SP-18},
 pages = {51--53},
 publisher = {航空宇宙技術研究所, National Aerospace Laboratory (NAL)},
 title = {Curvature effects in three-dimensional boundary layers},
 volume = {18},
 year = {1992}
}