activity
20182022
most citedTransonic aeroelasticity: a new perspective from the fluid mode

79 citations · 150 across the 12 of their papers we have counts for

collaborators

13 papers

physics.flu-dyn2022

Fast sparse flow field prediction around airfoils via multi-head perceptron based deep learning architecture

Kuijun Zuo, Shuhui Bu, Weiwei Zhang +3

In order to obtain the information about flow field, traditional computational fluid dynamics methods need to solve the Navier-Stokes equations on the mesh with boundary conditions…

physics.flu-dyn2021

High Reynolds number airfoil turbulence modeling method based on machine learning technique

Xuxiang Sun, Wenbo Cao, Yilang Liu +2

In this paper, a turbulence model based on deep neural network is developed for turbulent flow around airfoil at high Reynolds numbers. According to the data got from the Spalart-A…

physics.flu-dyn2021★ 27 cited

Analysis on numerical stability and convergence of RANS turbulence models from the perspective of coupling modes

Yilang Liu, Weiwei Zhang, Zhenhua Xia

Reynolds-averaged Navier-Stokes simulations are still the main method to study complex flows in engineering. However, traditional turbulence models cannot accurately predict flow f…

physics.flu-dyn2021★ 2 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-dyn2021★ 2 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…

eess.SP2020★ 6 cited

Machine Learning of Partial Differential Equations from Noise Data

Wenbo Cao, Weiwei Zhang

Machine learning of partial differential equations from data is a potential breakthrough to solve the lack of physical equations in complex dynamic systems, but because numerical d…

physics.flu-dyn2020★ 2 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-dyn2020★ 79 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.comp-ph2019★ 2 cited

Comparisons of Two Reduced-Order Models for Linearized Unsteady Aerodynamic Identification

Jiaqing Kou, Weiwei Zhang

This paper compares the performance of two unsteady aerodynamic reduced-order models (ROMs), namely linear Volterra series and the autoregressive with exogenous input (ARX) model,…

math.NA2019

Provably size-guaranteed mesh generation with superconvergence

Xiangrong Li, Nan Qi, Yufeng Nie +1

The properties and applications of superconvergence on size-guaranteed Delaunay triangulation generated by bubble placement method (BPM), are studied in this paper. First, we deriv…

physics.flu-dyn2018★ 9 cited

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★ 19 cited

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…

physics.comp-ph2018★ 2 cited

Mode Multigrid - A novel convergence acceleration method

Yilang Liu, Weiwei Zhang, Jiaqing Kou

This paper proposes a mode multigrid (MMG) method, and applies it to accelerate the convergence of the steady state flow on unstructured grids. The dynamic mode decomposition (DMD)…