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20182021
most citedTransonic aeroelasticity: a new perspective from the fluid mode

79 citations · 87 across the 5 of their papers we have counts for

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physics.flu-dyn20212 cited

Deep Learning for Multi-Fidelity Aerodynamic Distribution Modeling from Experimental and Simulation Data

Kai Li, Jiaqing Kou, Weiwei Zhang

The wind-tunnel experiment plays a critical role in the design and development phases of modern aircraft, which is limited by prohibitive cost. In contrast, numerical simulation, a…

physics.flu-dyn20212 cited

Experimental study on Vortex-Induced Vibration of Cylinder at Subcritical Reynolds Number

Zhen Lyu, Weiwei Zhang, Jiaqing Kou

Numerical simulation results in recent years show that vortex-induced vibration (VIV) can occur at a subcritical Reynolds number. And the VIV has been observed numerically at Reyno…

physics.flu-dyn20202 cited

A new data assimilation method of recovering turbulent flow field at high-Reynolds numbers for turbulence machine learning

Yilang Liu, Weiwei Zhang

This paper proposes a new data assimilation method for recovering high fidelity turbulent flow field around airfoil at high Reynolds numbers based on experimental data, which is ca…

physics.flu-dyn202079 cited

Transonic aeroelasticity: a new perspective from the fluid mode

Chuanqiang Gao, Weiwei Zhang

Within the transonic regime, the aeroelastic problems exhibit many unique characteristics compared with subsonic and supersonic cases. Although a lot of research has been carried o…

physics.flu-dyn2018

Machine learning methods for turbulence modeling in subsonic flows over airfoils

Weiwei Zhang, Linyang Zhu, Yilang Liu +1

Reynolds-Averaged Navier-Stokes(RANS) method will still play a vital role in the following several decade in aerospace engineering. Although RANS models are widely used, empiricism…

physics.flu-dyn2018

A novel unsteady aerodynamic Reduced-Order Modeling method for transonic aeroelastic optimization

Ziyi Wang, Weiwei Zhang, Xiaojing Wu +1

In aircraft design, structural optimization and uncertainty quantification concerning transonic aeroelastic issues are computationally impractical, because the iterative process re…