2021年
Experimental and Numerical Study of Hypersonic Flow over Backward-Facing Step
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
- ,
- ,
- 巻
- 19
- 号
- 5
- 開始ページ
- 735
- 終了ページ
- 743
- 記述言語
- 英語
- 掲載種別
- 研究論文(学術雑誌)
- DOI
- 10.2322/tastj.19.735
- 出版者・発行元
- Japan Society for Aeronautical and Space Sciences
Experimental and numerical studies were conducted to investigate the flow over a backward-facing step with finite aspect ratio. Measurements using pressure-sensitive paint, infrared thermal imaging, oil-flow visualization and schlieren imaging were conducted in the Hypersonic and High Enthalpy Wind Tunnel at the University of Tokyo. The results show the complex three-dimensional structure of the flow over a backward-facing step. The numerical simulation was also conducted, and the simulation results reveal that the fluid flow from the open side of the model has significant three-dimensional effect on the flow features. Comparison between CFD and experimental results is also made in this paper. A recirculation bubble found after the step, generated by the interaction of side expansion and recirculating flow, is observed in CFD results. A symmetric local peak pressure and heating region named ‘twin peak’ is also founded by both numerical simulation and experiments.
- リンク情報
- ID情報
-
- DOI : 10.2322/tastj.19.735
- eISSN : 1884-0485
- CiNii Articles ID : 130008084451
- CiNii Research ID : 1390852252714796544