An efficient large-scale mesh deformation method based on MPI/Open MP hybrid parallel radial basis function interpolation
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作者:
Zhong ZHAO
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机构:
State Key Laboratory of Aerodynamics, China Aerodynamics Research and Development Center
Computational Aerodynamics Institute, China Aerodynamics Research and Development CenterState Key Laboratory of Aerodynamics, China Aerodynamics Research and Development Center
Zhong ZHAO
[1
,2
]
Rong MA
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机构:
Computational Aerodynamics Institute, China Aerodynamics Research and Development CenterState Key Laboratory of Aerodynamics, China Aerodynamics Research and Development Center
Rong MA
[2
]
Lei HE
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机构:
Computational Aerodynamics Institute, China Aerodynamics Research and Development CenterState Key Laboratory of Aerodynamics, China Aerodynamics Research and Development Center
Lei HE
[2
]
Xinghua CHANG
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机构:
State Key Laboratory of Aerodynamics, China Aerodynamics Research and Development Center
Computational Aerodynamics Institute, China Aerodynamics Research and Development CenterState Key Laboratory of Aerodynamics, China Aerodynamics Research and Development Center
Xinghua CHANG
[1
,2
]
Laiping ZHANG
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机构:
State Key Laboratory of Aerodynamics, China Aerodynamics Research and Development Center
Computational Aerodynamics Institute, China Aerodynamics Research and Development CenterState Key Laboratory of Aerodynamics, China Aerodynamics Research and Development Center
Laiping ZHANG
[1
,2
]
机构:
[1] State Key Laboratory of Aerodynamics, China Aerodynamics Research and Development Center
[2] Computational Aerodynamics Institute, China Aerodynamics Research and Development Center
An efficient MPI/OpenMP hybrid parallel Radial Basis Function (RBF) strategy for both continuous and discontinuous large-scale mesh deformation is proposed to reduce the computational cost and memory consumption.Unlike the conventional parallel methods in which all processors use the same surface displacement and implement the same operation,the present method employs different surface points sets and influence radius for each volume point movement,accompanied with efficient geometry searching strategy.The deformed surface points,also called Control Points (CPs),are stored in each processor.The displacement of spatial points is interpolated by using only 20-50 nearest control points,and the local influence radius is set to 5-20 times the maximum displacement of control points.To shorten the searching time for the nearest control point clouds,an Alternating Digital Tree (ADT) algorithm for 3D complex geometry is designed based on an iterative bisection technique.Besides,an MPI/OpenMP hybrid parallel approach is developed to reduce the memory cost in each High-Performance Computing (HPC) node for large-scale applications.Three 3D cases,including the ONERA-M6 wing and a commercial transport airplane standard model with up to 2.5 billion hybrid elements,are used to test the present mesh deformation method.The robustness and high parallel efficiency are demonstrated by a wing deflection case with a maximum bending angle of 450 and more than 80% parallel efficiency with 1024 MPI processors.In addition,the availability for both continuous and discontinuous surface deformation is verified by interpolating the projecting displacement with opposite directions surface points to the spatial points.
机构:
China Aerodynam Res & Dev Ctr, State Key Lab Aerodynam, Mianyang 621000, Sichuan, Peoples R China
China Aerodynam Res & Dev Ctr, Computat Aerodynam Inst, Mianyang 621000, Sichuan, Peoples R ChinaChina Aerodynam Res & Dev Ctr, State Key Lab Aerodynam, Mianyang 621000, Sichuan, Peoples R China
Zhao, Zhong
Ma, Rong
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China Aerodynam Res & Dev Ctr, Computat Aerodynam Inst, Mianyang 621000, Sichuan, Peoples R ChinaChina Aerodynam Res & Dev Ctr, State Key Lab Aerodynam, Mianyang 621000, Sichuan, Peoples R China
Ma, Rong
He, Lei
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China Aerodynam Res & Dev Ctr, Computat Aerodynam Inst, Mianyang 621000, Sichuan, Peoples R ChinaChina Aerodynam Res & Dev Ctr, State Key Lab Aerodynam, Mianyang 621000, Sichuan, Peoples R China
He, Lei
Chang, Xinghua
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机构:
China Aerodynam Res & Dev Ctr, State Key Lab Aerodynam, Mianyang 621000, Sichuan, Peoples R China
China Aerodynam Res & Dev Ctr, Computat Aerodynam Inst, Mianyang 621000, Sichuan, Peoples R ChinaChina Aerodynam Res & Dev Ctr, State Key Lab Aerodynam, Mianyang 621000, Sichuan, Peoples R China
Chang, Xinghua
Zhang, Laiping
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机构:
China Aerodynam Res & Dev Ctr, State Key Lab Aerodynam, Mianyang 621000, Sichuan, Peoples R China
China Aerodynam Res & Dev Ctr, Computat Aerodynam Inst, Mianyang 621000, Sichuan, Peoples R ChinaChina Aerodynam Res & Dev Ctr, State Key Lab Aerodynam, Mianyang 621000, Sichuan, Peoples R China
机构:
School of Aeronautics, Northwestern Polytechnical University, Xi’an,710072, China
AVIC Shenyang Aircraft Design and Research Institute, Shenyang,110035, ChinaSchool of Aeronautics, Northwestern Polytechnical University, Xi’an,710072, China
Lu, Kuan
Song, Wenping
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机构:
School of Aeronautics, Northwestern Polytechnical University, Xi’an,710072, China
National Key Laboratory of Aircraft Configuration Design, Xi’an,710072, ChinaSchool of Aeronautics, Northwestern Polytechnical University, Xi’an,710072, China
Song, Wenping
Guo, Hengbo
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机构:
School of Aeronautics, Northwestern Polytechnical University, Xi’an,710072, China
National Key Laboratory of Aircraft Configuration Design, Xi’an,710072, ChinaSchool of Aeronautics, Northwestern Polytechnical University, Xi’an,710072, China
Guo, Hengbo
Ye, Kun
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机构:
School of Aeronautics, Northwestern Polytechnical University, Xi’an,710072, China
National Key Laboratory of Aircraft Configuration Design, Xi’an,710072, ChinaSchool of Aeronautics, Northwestern Polytechnical University, Xi’an,710072, China
Ye, Kun
Wang, Yue
论文数: 0引用数: 0
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机构:
School of Aeronautics, Northwestern Polytechnical University, Xi’an,710072, China
National Key Laboratory of Aircraft Configuration Design, Xi’an,710072, ChinaSchool of Aeronautics, Northwestern Polytechnical University, Xi’an,710072, China
Wang, Yue
Han, Zhonghua
论文数: 0引用数: 0
h-index: 0
机构:
School of Aeronautics, Northwestern Polytechnical University, Xi’an,710072, China
National Key Laboratory of Aircraft Configuration Design, Xi’an,710072, ChinaSchool of Aeronautics, Northwestern Polytechnical University, Xi’an,710072, China
Han, Zhonghua
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica,
2024,
45
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