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Knowledge Management System of Institue of Mechanics, CAS
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杨国伟 [4]
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Parametric study on wing-lambda-shock formation
会议论文
Fluids Engineering Division Summer Meeting, FEDSM 2021, Virtual, Online, 10 August 2021 到 12 August 2021
Authors:
Chainok S
;
Rungroch T
;
Chairach P
;
Prapamonthon P
;
Yooyen S
;
Yin B(银波)
;
Yang GW(杨国伟)
;
Ju SJ(鞠胜军)
Adobe PDF(3026Kb)
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View/Download:302/97
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Submit date:2021/11/30
Shock
Supersonic flow
Transonic flow
Fixed-Point Fluid structure interaction analysis BASED ON geometrically exact approach
期刊论文
SCIENTIFIC REPORTS, 2020, 卷号: 10, 期号: 1, 页码: 16
Authors:
Yu ML(余明亮)
;
Nie XY(聂雪媛)
;
Yang GW(杨国伟)
;
Zhong PN(钟培楠)
Adobe PDF(4371Kb)
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View/Download:303/97
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Submit date:2020/08/26
Time efficient aeroelastic simulations based on radial basis functions
期刊论文
JOURNAL OF COMPUTATIONAL PHYSICS, 2017, 卷号: 330, 页码: 810-827
Authors:
Liu W(刘文)
;
Huang CD(黄程德)
;
Yang GW(杨国伟)
;
Liu, W (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100190, Peoples R China.
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Submit date:2017/04/26
Response Surface Technique for Static Aeroelastic Optimization on a High-Aspect-Ratio Wing
期刊论文
Journal of Aircraft, 2009, 卷号: 46, 期号: 4, 页码: 1444-1450
Authors:
Yang GW(杨国伟)
;
Chen DW(陈大伟)
;
Cui K(崔凯)
;
Yang GW
Adobe PDF(1016Kb)
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Submit date:2009/08/03
Navier-stokes Solver
Aircraft