@techreport{oai:jaxa.repo.nii.ac.jp:00043154,
 author = {小屋, 雅彦 and 小竹, 進 and Koya, Masahiko and Kotake, Susumu},
 month = {Nov},
 note = {In order to calculate higher subsonic or transonic flows in highly three-dimensionally twisted turbine blade cascades, the finite volume integral method of solving the governing equations is implemented for the treatment of boundary conditions and the discretization scheme. The scheme developed here reduces the discretization error associated with the distorted grid configuration of highly three-dimensional blades. With the developed method, flows in three typical turbine blade cascades have been calculated. The present scheme can be applied to a fully three-dimensional flow through complete turbine stages., 資料番号: NALSP0003012, レポート番号: NAL SP-3},
 title = {遷音速タービン翼間流れ三次元解析},
 year = {1984}
}