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Knowledge Management System of Institue of Mechanics, CAS
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Funding Project：National Natural Science Foundation of China[11702298]
Document Type：期刊论文
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Aeroelastic Simulation Using CFD/CSD Coupling Based on Precise Integration Method
期刊论文
INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, 2020, 页码: 18
Authors:
Huang CD(黄程德)
;
Huang J(黄杰)
;
Song X(宋鑫)
;
Zheng GN(郑冠男)
;
Nie XY(聂雪媛)
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Submit date：2020/04/07
Flutter
Static aeroelasticity
CFD
CSD coupling
Precise integration method
