Rotorcraft fuselage and ship airwakes simulations using an immersed boundary method
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Park, H.S.
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School of Aerospace, Mechanical and Mechatronic Engineering, The University of Sydney, Sydney,New South Wales,2006, AustraliaSchool of Aerospace, Mechanical and Mechatronic Engineering, The University of Sydney, Sydney,New South Wales,2006, Australia
Park, H.S.
[1
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Linton, D.
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School of Aerospace, Mechanical and Mechatronic Engineering, The University of Sydney, Sydney,New South Wales,2006, AustraliaSchool of Aerospace, Mechanical and Mechatronic Engineering, The University of Sydney, Sydney,New South Wales,2006, Australia
Linton, D.
[1
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Thornber, B.
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School of Aerospace, Mechanical and Mechatronic Engineering, The University of Sydney, Sydney,New South Wales,2006, AustraliaSchool of Aerospace, Mechanical and Mechatronic Engineering, The University of Sydney, Sydney,New South Wales,2006, Australia
Thornber, B.
[1
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机构:
[1] School of Aerospace, Mechanical and Mechatronic Engineering, The University of Sydney, Sydney,New South Wales,2006, Australia
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;
机构:
Zhejiang Univ, State Key Lab Clean Energy Utilizat, Hangzhou 310027, Peoples R ChinaZhejiang Univ, State Key Lab Clean Energy Utilizat, Hangzhou 310027, Peoples R China
Luo, Kun
Wang, Zeli
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Zhejiang Univ, State Key Lab Clean Energy Utilizat, Hangzhou 310027, Peoples R ChinaZhejiang Univ, State Key Lab Clean Energy Utilizat, Hangzhou 310027, Peoples R China
Wang, Zeli
Fan, Jianren
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Zhejiang Univ, State Key Lab Clean Energy Utilizat, Hangzhou 310027, Peoples R ChinaZhejiang Univ, State Key Lab Clean Energy Utilizat, Hangzhou 310027, Peoples R China