@techreport{oai:jaxa.repo.nii.ac.jp:00043252,
 author = {宮川, 淳一 and 高梨, 進 and 藤井, 孝蔵 and 天野, 完一 and Miyakawa, Jun-ichi and Takanashi, Susumu and Fujii, Kozo and Amano, Kan-ichi},
 month = {Dec},
 note = {Computational aerodynamics has evolved to the point where it has become a practical design tool comparable to wind tunnel tesing and has played an important role in actual aircraft design stages. The Navier-Stokes code, however, is still restricted to two-dimensional applications, which have been repeatedly validated in this symposium. The three-dimensional application, which is a real challenge for the Navier-Stokes code, is discussed in this paper for the first time, If this three-dimensional application could be perfected, it would be a big step toward the final target of complete aircraft analysis by numerical simulation., 資料番号: NALSP0007036, レポート番号: NAL SP-7},
 title = {遷音速機の数値シミュレーションと風洞試験の対応},
 year = {1986}
}