@techreport{oai:jaxa.repo.nii.ac.jp:00043229,
 author = {丸山, 祐一 and 秋下, 貞夫 and 中村, 昭人 and Maruyama, Yuichi and Akishita, Sadao and Nakamura, Akihito},
 month = {Dec},
 note = {Steady supersonic linearized potential flows about two types of wings and a wing-body configuration were simulated using the panel method program MARCAP. Linearly varying doublet distribution is adopted to ensure the continuity of the strength on panel edges, while constant distribution on each panel is used for source. Morino's scheme is employed for most cases. The velocity boundary condition scheme is also applied to some cases. The results show good agreement with analytical solutions and wind tunnel testings. The computation time is within a reasonable limit, and the program size is comparable to those of panel methods for incompressible or subsonic flows., 資料番号: NALSP0007013, レポート番号: NAL SP-7},
 title = {パネル法による超音速流の数値解析},
 year = {1986}
}