開口端をもつ管内からの衝撃波放出
| العنوان: | 開口端をもつ管内からの衝撃波放出 |
|---|---|
| المؤلفون: | Onishi, Yoshimoto, Oshida, Takeshi, Okada, Hiroki, Nakajima, Takashi |
| المصدر: | 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. :75-78 |
| بيانات النشر: | 宇宙航空研究開発機構宇宙科学研究本部, 2004. |
| سنة النشر: | 2004 |
| مصطلحات موضوعية: | noise reduction, shock wave, 衝撃波, Astrophysics::High Energy Astrophysical Phenomena, 騒音低減, 粘性流, 圧縮性流体, Navier-Stokes方程式, viscous flow, shock wave propagation, Navier-Stokes equation, 数値シミュレーション, compressible fluid, gas viscosity, vortex ring, numerical simulation, 気体粘度, 渦輪, 衝撃波伝播 |
| الوصف: | 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 |
| اللغة: | Japanese |
| الوصول الحر: | https://explore.openaire.eu/search/publication?articleId=jairo_______::ae7c64e508c12ff3c8f4e51b68feeea7Test http://id.nii.ac.jp/1696/00014659Test/ |
| رقم الانضمام: | edsair.jairo.........ae7c64e508c12ff3c8f4e51b68feeea7 |
| قاعدة البيانات: | OpenAIRE |
| الوصف غير متاح. |