@techreport{oai:jaxa.repo.nii.ac.jp:00043226,
 author = {高梨, 進 and 田村, 敦宏 and 中村, 孝 and 広瀬, 直喜 and Takanashi, Susumu and Tamura, Atsuhiro and Nakamura, Takashi and Hirose, Naoki},
 month = {Dec},
 note = {In this paper, a simple and practical inverse design method is described for two-dimensional transonic cascades with specified target distributions. The present design procedure is based on an iterative residual correction concept. The difference between target and computed pressures, at each iteration step, is deter-mined using a cascade analysis code. The blade surface correction corresponding to the pressure difference (or residual) is approximately obtained by transonic integral equa-tions. Typical examples designed by the present method using the full potential solver as the analysis code are presented for subsonic and transonic cascades with specified pressures., 資料番号: NALSP0007010, レポート番号: NAL SP-7},
 title = {逆解法による翼列設計},
 year = {1986}
}