Wall-modeled large eddy simulation of the A-airfoil using body-fitted and immersed-boundary codes

被引：0

作者：

Hussain, Md Daluar ^{[1
]}

Ganju, Sparsh ^{[2
]}

Batstone, Joshua ^{[3
]}

Brehm, Christoph ^{[3
]}

Larsson, Johan ^{[1
]}

van Noordt, William ^{[4
,5
]}

机构：

[1] Univ Maryland, Dept Mech Engn, College Pk, MD 20742 USA

[2] Univ Maryland, College Pk, MD 20742 USA

[3] Univ Maryland, Dept Aerosp Engn, College Pk, MD 20742 USA

[4] Whoosh HPC Lab, Kensington, MD 20895 USA

[5] Univ Oxford, Oxford OX1 3PJ, England

来源：

AIAA AVIATION FORUM AND ASCEND 2024 | 2024年

关键词：

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The paper presents wall-modeled large eddy simulations (WMLES) of the flow over an airfoil using two codes, with specific focus on comparing the results using body-fitted grids and Cartesian grids with immersed-boundary treatment and on how to handle the laminar boundary layer at the leading edge of the airfoil. The study highlights the difficulty of handling the extremely thin laminar boundary layer around the leading edge and how this affects the boundary layer over the entire airfoil, leading to changes in the predicted lift and drag.

引用

页数：11

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