@article{oai:jaxa.repo.nii.ac.jp:00031952,
 author = {服部, 直三 and 八田, 桂三 and 小竹, 進 and Hattori, Naozo and Hatta, Keizo and Kotake, Susumu},
 issue = {4},
 journal = {東京大学宇宙航空研究所報告},
 month = {Oct},
 note = {タービンディスクの冷却に関して問題となる回転円板の熱伝達機構を,円板中心から半径方向への空気の流れおよび円板周辺における軸方向への高温ガスの流れの中におかれた回転円板に対して実験的に研究した.回転円板の表面温度分布および円板周囲の温度分布を熱電対を用いて測定し,得られた温度分布曲線から円板周囲の流れおよび熱伝達の様子を推定した., The mechanism of the heat transfer from a rotating disk which is actually very important problem on the cooling of a turbine disk was investigated experimentally with a disk rotated in a closed space, cooled by the radial outward air flow on the surface and heated by the axial hot gas flow at the rim. The temperature distribution on the surface of the disk and in the closed space were measured using thermocouples to presume the flow pattern and the heat transfer., 資料番号: SA0125024000},
 pages = {564--581},
 title = {回転円板の熱伝達について},
 volume = {3},
 year = {1967}
}