@article{oai:ir.kagoshima-u.ac.jp:00000828,
 author = {宮里, 義昭 and Miyazato, Yoshiaki and 樫谷, 賢士 and Kashitani, Masashi and 金, 羲東 and Kim, Heuy-Dong and 片野田, 洋 and Katanoda, Hiroshi and 松尾, 一泰},
 issue = {607},
 journal = {日本機械学會論文集. B編},
 month = {},
 note = {Experiments on the shock wave/turbulent boundary layer interaction were conducted at the free  stream Mach number M1e of 1.97 to 2.50 and the Reynolds number based on the boundary layer  thickness Reδ1 of 3.1 x 10^4 to 5.8 x 10^4 using a supersonic nozzle having a divergent half angle of 10 degrees. Nozzle wall static pressure measurements and the schlieren optical observation of the  interaction region were carried out. Also, the effects of M1e and Reδ1 on the shock-induced turbulent  boundary layer separation were investigated theoretically. As a result, the analytical results of the ratio Ps/P1 of the eparation pressure Ps to the pressure at the onset of the interaction P1 were found to increase with increasing M1e for a fixed Reδ1 and to increase with increasing Reδ1 for a fixed M1e and to provide excellent agreement with the experimental results on the shock-induced turbulent 
 boundary layer separation.},
 pages = {879--886},
 title = {超音速ノズル内の衝撃波による乱流境界層のはく離},
 volume = {63},
 year = {1997},
 yomi = {ミヤザト, ヨシアキ and カシタニ, マサシ and カタノダ, ヒロシ}
}