@techreport{oai:jaxa.repo.nii.ac.jp:00043138,
 author = {高梨, 進 and Takanashi, Susumu},
 month = {Nov},
 note = {A numerical design procedure for three-dimensional transonic wings is presented. In this method, the boundary value problem is solved for the wing geometry which induces a prescribed pressure distribution subject to additional requirements on trailing-edge closure. The method is based on the transonic small disturbance theory and utilizes a type-dependent relaxation technique. Design results for large aspect ratio supercritical swept wings are also presented., 資料番号: NALSP0001020, レポート番号: NAL SP-1},
 title = {三次元遷音速翼の設計},
 year = {1983}
}