@techreport{oai:jaxa.repo.nii.ac.jp:00043533,
 author = {穂刈, 高志 and 斎藤, 茂 and 田中, 厚成 and 竹内, 久雄 and 松永, 康二 and 菊地, 一雄 and 田村, 敦宏 and Hokari, Takashi and Saito, Shigeru and Tanaka, Atsushige and Takeuchi, Hisao and Matsunaga, Koji and Kikuchi, Kazuo and Tamura, Atsuhiro},
 month = {Dec},
 note = {Numerical simulation for the cascade of aeroengine is usually done about circumferentical same airfoils and is one-pitch calculation. but in the real engine there are little changed airfoil or structures between cascade. So, we extended one-pitch calculation code to multiple-pitch and named it analysis of non-uniform airfoil cascade. In this paper we use this code to bypass duct of a commercial jet engine and get good agreement between analysis and experiment., 資料番号: NALSP0016037, レポート番号: NAL SP-16},
 title = {多翼素翼列まわりの流れの数値シミュレーション},
 year = {1991}
}