@techreport{oai:jaxa.repo.nii.ac.jp:00043312,
 author = {海田, 武司 and 宮川, 淳一 and 柳沢, 三憲 and 天野, 完一 and Kaiden, Takeshi and Miyakawa, Jun-ichi and Yanagisawa, Mitsunori and Amano, Kan-ichi},
 month = {Dec},
 note = {The rapid progress of the computational aerodynamics enables us to analyze airflow with viscous calculation instead of with invisid one. In two-dimensional application, we have already validated its effectiveness in comparison with wind tunnel testing and put it into practical stage. In three-dimensional application, the wing-body configulation has been also done. This paper presents a validative discussion of the panel method toward the analysis about the complete aircraft, including the calculation of the sting interference, which is indispensable to wind tunnel testing. The results indicate that the panel method is valid in the subsonic region and that the sting makes up wash flow., 資料番号: NALSP0009021, レポート番号: NAL SP-9},
 title = {遷音速全機形状まわりのパネル法計算と風洞試験の比較},
 year = {1988}
}