@article{oai:jaxa.repo.nii.ac.jp:00032613,
 author = {長島, 利夫 and 谷田, 好通 and NAGASHIMA, Toshio and TANIDA, Yoshimichi},
 issue = {1_A},
 journal = {東京大学宇宙航空研究所報告},
 month = {Feb},
 note = {Searsによる翼のガスト応答の問題を,亜音速流れ中でexp[iω(t-x/V)+iλz]と表わされる3次元的ガストに拡張し,特異点法を用いて解いた.翼の前縁に対してガスト波面が傾斜する効果が大きいことが結論された., The Sears type lift functions (Imaginery vs. real parts of the unsteady lift coefficient) of an aerofoil operating in sinusoidal gusts of a general form: exp[iω (t-x/V) + iλz)] with a subsonic flow have been calculated. The obliqueness of the gust wave front with respect to the aerofoil leading edge is found to be very influencial upon the aerodynamic lift and moment., 資料番号: SA0125949000},
 pages = {23--34},
 title = {<論文>圧縮流れ中の翼のガスト応答と傾斜効果},
 volume = {17},
 year = {1981}
}