@techreport{oai:jaxa.repo.nii.ac.jp:00043446,
 author = {新田, 恭子 and 安東, 茂典 and 和久, 浩行 and Nitta, Kyoko and Ando, Shigenori and Waku, Hiroshi},
 month = {Nov},
 note = {The lift on an airfoil flying over a wavy wall surface is calculated using a finite difference method, which was developed by J. Nakamichi1) to improve LTRAN2 evolved by W.F. Ballhaus & P.M. Goorjian2). Numerical computations include cases of a flat plate over a flat solid wall prior to the cases of a moving wavy wall. Modification of grid generating system is the major point for applying Nakamichi's method to our problem. The weak compressibility (M infinity =0.1-0.3) is considered but non-linearity is neglected in our calculations. The calculated results are compared with those obtained by the lifting surface theory of M. Ichikawa et al.3) The agreements are quite satisfactory., 資料番号: NALSP0014013, レポート番号: NAL SP-14},
 title = {波状壁面上を飛ぶ2次元翼空力荷重の差分法による計算},
 year = {1990}
}