@article{oai:jaxa.repo.nii.ac.jp:00031590,
 author = {小口, 伯郎 and 船曳, 勝之 and 佐藤, 俊逸 and OGUCHI, Hakuro and FUNABIKI, Katsushi and SATO, Shunitsu},
 issue = {4_B},
 journal = {東京大学宇宙航空研究所報告},
 month = {Jan},
 note = {This paper reports the performance and flow characteristics of the shock tube equipped ,with a shock wave valve, which is modified in more feasible fashion for practical use from one previously proposed by Muirhead et al. In order to clarify the starting processes of the multiple nozzles, an experiment was conducted by means of this shock tube to observe the feature of the flow accompanying with the shock waves reflected from and passing through the multiple-orifice plate set normal to the flow at the test section., 資料番号: SA0124542000},
 pages = {3--10},
 title = {無隔膜衝撃波管による多孔板と衝撃波の干渉に関する実験},
 volume = {11},
 year = {1976}
}