@techreport{oai:jaxa.repo.nii.ac.jp:00043351,
 author = {藤, 秀実 and 佐藤, 幸徳 and 安藤, 安則 and 河合, 理文 and Toh, Hidemi and Sato, Yukinori and Ando, Yasunori and Kawai, Masafumi},
 month = {Nov},
 note = {Aerothermal analysis for gas turbine combustion liner cooling slots is presented. A finite-volume numerical analysis method for the solution of three-dimensional incompressible steady Navier-Stokes equations in general curvilinear coordinate system is used for the analysis. The main solution algorithm of the method is an extension of SIMPLE algorithm to present general curvilinear coordinate formulation. The standard k-epsilon two equations is used for turbulence model. This method is applied to calculate the velocity, temperature, liner skin temperature distributions and cooling effectiveness. Effects of combustion liner cooling slot configuration on such distributions were examined., 資料番号: NALSP0010022, レポート番号: NAL SP-10},
 title = {ガスタービン燃焼器ライナ冷却部の伝熱解析},
 year = {1989}
}