Xiaohui SU
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Numerical simulation of 3D rigid wing hovering flight
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Indexed by:会议论文

Date of Publication:2019-01-01

Included Journals:EI

Volume:1300

Issue:1

Abstract:In this paper, we propose a new CFD numerical simulation method, which combines the ALE program independently developed by our research group and commercial software CFX. The feasibility and accuracy of this CFD method are verified by simulating hovering flight of 3D rigid wing. By analyzing the flow field, it is believed that LEV attached to the upper surface of the wing is the main reason for generating large lift during downstroke, and delayed stall mechanism play a important role.

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Gender:Male

Alma Mater:大连理工大学

Degree:Doctoral Degree

School/Department:水利工程系

Discipline:Hydraulic Structure Engineering. Hydraulics and River Dynamics. Fluid Machinery and Engineering

Business Address:大连理工大学建设工程学部水利学院
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