@article{oai:muroran-it.repo.nii.ac.jp:00008351,
 author = {杉山,  弘 and SUGIYAMA, Hiromu and 溝端,  一秀 and MIZOBATA, Kazuhide and 新井,  隆景 and ARAI, Takakage and 福田,  浩一 and FUKUDA, Koichi and 孫,  立群 and SUN, Li Qun and 遠藤,  清和 and ENDO, Kiyokazu and 広島,  敬之 and HIROSHIMA, Takayuki},
 journal = {室蘭工業大学紀要, Memoirs of the Muroran Institute of Technology},
 month = {Nov},
 note = {application/pdf, To investigate the supersonic flow phenomena related to internal and external flows of high-pressure gas pipeline systems, new air breathing engines and space planes, a new supersonic wind tunnel (pressure - vacuum type, Mach4.0 and 2.0) was designed and constructed in Muroran Institute of Technology (MIT). This paper describes the flow characteristics of the Mach 4 and 2 supersonic wind tunnel and the experimental study on the shock wave and turbulent boundary layer interactions (pseudo-shock wave, or PSW) in a rectangular duct, using the MIT supersonic wind tunnel., 小特集 : 「室蘭工大における航空宇宙工学研究の新展開」},
 pages = {57--62},
 title = {室蘭工業大学新設マッハ4超音速風洞の気流特性および衝撃波と乱流境界層の干渉現象に関する研究},
 volume = {51},
 year = {2001},
 yomi = {スギヤマ, ヒロム and ミゾバタ, カズヒデ and アライ, タカカゲ and フクダ, コウイチ and エンドウ, キヨカズ and ヒロシマ, タカユキ}
}