LES of hypersonic flow over a 3D single-fin

Fang, Jian; Yao, Yufeng; Lu, Lipeng; Zheng, Yao

Abstract

LES of hypersonic flow passing a 3D single-fin at Mach 5 and Re∞=3.7×107/m was conducted using a newly developed 7th-order low-dissipation monotonicity-preserving NS solver with dynamic Smagorinsky subgrid model. The simulation captures salient flow phenome such as shock systems, flow separation structures, and turbulence characteristics. It was found that in the reverse flow region, the streamwise elongated coherent structures are regenerated beneath the main separation vortex, almost immediately after the flow reattachment.

Citation

Fang, J., Yao, Y., Lu, L., & Zheng, Y. (2015, July). LES of hypersonic flow over a 3D single-fin. Presented at The First Chinese International Conference on CFD, Mianyang, China

• Presentation Conference Type: Keynote
• Conference Name: The First Chinese International Conference on CFD
• Conference Location: Mianyang, China
• Start Date: Jul 15, 2015
• End Date: Jul 16, 2015
• Publication Date: Jul 15, 2015
• Publicly Available Date: Jun 6, 2019
• Peer Reviewed: Not Peer Reviewed
• Keywords: LES, hypersonic flow, single-fin
• Public URL: https://uwe-repository.worktribe.com/output/831189
• Additional Information: Title of Conference or Conference Proceedings : The First Chinese International Conference on CFD