@techreport{oai:jaxa.repo.nii.ac.jp:00043368,
 author = {宮川, 淳一 and 高梨, 進 and Miyakawa, Jun-ichi and Takanashi, Susumu},
 month = {Nov},
 note = {Computational aerodynamics has evolved to be a practical design tool comparable to wind tunnel testing, and it has played an important role in actual aircraft design stages. There have been intensive works already done for code validation to support the accuracy of the computation. This paper adds another effort to those works by discussing the code accuracy based upon comparison between numerical simulation and actual flight test which has never been done before., 資料番号: NALSP0010039, レポート番号: NAL SP-10},
 title = {小型高速機主翼圧力分布の数値シミュレーションと飛行試験の比較},
 year = {1989}
}