@techreport{oai:jaxa.repo.nii.ac.jp:00043451,
 author = {谷, 泰寛 and 越岡, 康弘 and 廣瀬, 秀大 and Tani, Yosuhiro and Koshioka, Yasuhiro and Hirose, Hidehiro},
 month = {Nov},
 note = {In this paper, an iterative design procedure is described for three dimensional wing-body configuration, especially blended wing-body configuration, using a three dimensional transonic inverse method with target pressure distribution. In this application, it is combined with a full potential analysis code. Some of the design results for a conventional and a blended wing-body configuration are presented. Also a finite volume Euler solver is applied to analyze the designed configurations., 資料番号: NALSP0014018, レポート番号: NAL SP-14},
 title = {逆解法を用いた翼胴一体化設計について},
 year = {1990}
}