@article{oai:muroran-it.repo.nii.ac.jp:00008350,
 author = {咲間,  文順 and SAKIMA, Fuminori and 新井,  隆景 and ARAI, Takakage and 笠原,  次郎 and KASAHARA, Jiro and 何,  斐 and HE, Fei and 阿弥,  貴之 and AMI, Takayuki},
 journal = {室蘭工業大学紀要, Memoirs of the Muroran Institute of Technology},
 month = {Nov},
 note = {application/pdf, Transverse sonic jet (nitrogen) was injected from a circular injector on an inclined fiat plate into a supersonic cross flow. Flow characteristics of a jet was organized by a penetration height of jet depended on the jet-to-freestream momentum flux ratio. The resuｌts showed that the penetration height was proportional to thejet-tｏ-freestream momentum flux ratio to the power of 0.68 (M1 = 1.7) or 0.70 (M1 = 3.3). Furthermore, in order to investigate the interaction between boundary layer on the flat plate and shock wave generated by the transverse sonic jet, chamcteristics of separated boundary layer and bow shock wave were observed. The separated boundary layer region and scale of bow shock could be found to be increased as the jet-to-freestream momentum flux ratio increased. The results also showed that the shock wave/boundary layer interaction had influenced on the penetration height of jet., 小特集 : 「室蘭工大における航空宇宙工学研究の新展開」},
 pages = {63--68},
 title = {超音速流中に垂直に噴出する音速噴流の挙動},
 volume = {51},
 year = {2001},
 yomi = {サキマ, フミノリ and アライ, タカカゲ and カサハラ, ジロウ and アミ, タカユキ}
}