@inproceedings{oai:jaxa.repo.nii.ac.jp:00014665,
 author = {大西, 善元 and 大信田, 丈志 and 岡田, 裕貴 and 中島, 俊 and Onishi, Yoshimoto and Oshida, Takeshi and Okada, Hiroki and Nakajima, Takashi},
 book = {宇宙航行の力学シンポジウム　平成15年度, Symposium on Flight Mechanics and Astrodynamics 2003},
 month = {May},
 note = {The behavior of a shock wave emitted from an open end of a shock tube is studied for 2-dimensional cases (where the tube is a channel) and for 3-dinensional cases (where the tube is a circular pipe). Attention is focused on the effects of finite viscosity and heat conductivity. In the present case, the shock wave has a finite thickness and is emitted in a fairly isotropic way. The decay law of the emitted shock, nearly spherical or cylindrical, is numerically investigated., 資料番号: AA0047120020},
 pages = {75--78},
 publisher = {宇宙航空研究開発機構宇宙科学研究本部, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)},
 title = {開口端をもつ管内からの衝撃波放出},
 year = {2004}
}