| タイトル | 曲面板に沿う超音速噴流のコアンダ現象の解明 |
| その他のタイトル | Analysis of the Coanda effect of the supersonic jet along curved surface wall |
| 著者（日） | 児島 忠倫; 篠塚 晃裕; 矢納 陽 |
| 著者（英） | Kojima, Tadatomo; Shinozuka, Akihiro; Yano, Akira |
| 著者所属（日） | 近畿大学 工学部 システムデザイン工学科; 近畿大学 大学院工業技術研究科; 近畿大学 工学部 システムデザイン工学科 |
| 著者所属（英） | Kinki University Department of System Design Engineering, School of Engineering; Kinki University Graduate School of Industrial Technology; Kinki University Department of System Design Engineering, School of Engineering |
| 発行日 | 2005-12-20 |
| 発行機関など | 近畿大学工学部
School of Engineering, Kinki University |
| 刊行物名 | 近畿大学工学部研究報告
Research Reports of the School of Engineering, Kinki University |
| 号 | 39 |
| 開始ページ | 161 |
| 終了ページ | 165 |
| 刊行年月日 | 2005-12-20 |
| 言語 | jpn |
| 抄録 | It is very meaningful that the Coanda effect is one of the characters of the jet flow, which clarifies the structure and behavior from the viewpoint of technological application. Recently, the numerical analysis and the experiment have been studied for the subsonic flow, but almost have not been researched for the supersonic flow. Then, the jet flow was issued from an asymmetric nozzle with an oblique outlet, the structure of the Coanda effect of the supersonic flow along curved surface wall was clarified, and the process where the Coanda effect was caused by the numerical analysis was clarified in this research too. As a result, it was able to be confirmed that the experiment and the numerical analysis were corresponding well. In addition, the Coanda effect of a supersonic flow through the numerical analysis was studied. |
| キーワード | flow visualization; supersonic jet flow; Coanda effect; numerical analysis; Mach number; curved surface wall; asymmetric nozzle; 流れの可視化; 超音速噴流; コアンダ効果; 数値解析; マッハ数; 曲面板; 非対称ノズル |
| 資料種別 | Technical Report |
| ISSN | 0386-491X |
| SHI-NO | AA0048639001 |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/36920 |
