Rotorcraft fuselage and ship airwakes simulations using an immersed boundary method

被引：0
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作者：
Park, H.S. [1 ]
Linton, D. [1 ]
Thornber, B. [1 ]
机构：
[1] School of Aerospace, Mechanical and Mechatronic Engineering, The University of Sydney, Sydney,New South Wales,2006, Australia
来源：
International Journal of Heat and Fluid Flow | 2022年 / 93卷
关键词：
The authors acknowledge the University of Sydney high performance computing (HPC) cluster Artemis and the National Computational Infrastructure HPC system Gadi for providing the HPC resources that have contributed to the research results reported within this paper;
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