@conference { , title = {LES of hypersonic flow over a 3D single-fin}, 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after the flow reattachment.}, conference = {The First Chinese International Conference on CFD}, publicationstatus = {Unpublished}, url = {https://uwe-repository.worktribe.com/output/831189}, keyword = {Engineering Modelling and Simulation Research Group, LES, hypersonic flow, single-fin}, year = {2015}, author = {Fang, Jian and Yao, Yufeng and Lu, Lipeng and Zheng, Yao} }