@techreport{oai:jaxa.repo.nii.ac.jp:00043354,
 author = {野崎, 理 and 田村, 敦宏 and 渡辺, 紀徳 and 金沢, 功 and Nozaki, Osamu and Tamura, Atsuhiro and Watanabe, Toshinori and Kanazawa, Isao},
 month = {Nov},
 note = {Three dimensional viscous flowfield through a linear turbine blade row with tip clearance leak age was numerically simulated. Flowfield was decomposed to a H-grid region on the blade tip and a C-grid one around it. Navier-Stokes equations were solved in each of them and the boundary conditions between them were connected with each other. In case of low incidence angle, the computed results for the total pressure loss in a downs tream section and limiting stream lines in a horizontal section showed qualitatively good agreement with experimental data., 資料番号: NALSP0010025, レポート番号: NAL SP-10},
 title = {翼端間隙を有するタービン翼列の流れ解析},
 year = {1989}
}