Weigang Yao

Senior Lecturer in Aeronautical Engineering

De Montfort University

United Kingdom

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Dr. Weigang Yao is a Senior Lecturer in Aeronautical Engineering at De Montfort University, UK. His research focuses on advanced aerodynamics, as evidenced by his recent articles which explore topics such as lift enhancement in flexible airfoils, aerodynamic shape design optimization, and data-driven model-order reduction techniques. He is particularly interested in utilizing neural networks and dynamic modeling to improve aerodynamic performance and efficiency.

Articles (19)

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2025

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2020

Collaborators (4)

Hossein Malekmohamadi

De Montfort University

UNITED KINGDOM

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Liang Sun

Lecturer

University of Ulster

UNITED KINGDOM

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Simão Marques

Senior Lecturer

University of Surrey

UNITED KINGDOM

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Trevor Robinson

The Queen's University Belfast

UNITED KINGDOM

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Weigang Yao

Research Interests

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Articles (19)

Modal Phase Study on Lift Enhancement of a Locally Flexible Membrane Airfoil Using Dynamic Mode Decomposition

Manifold Learning for Aerodynamic Shape Design Optimization

Enhancing the Goman–Khrabrov dynamic stall model through flow delay analysis

Utilizing global-local neural networks for the analysis of non-linear aerodynamics

Data-driven reduced-order modeling for nonlinear aerodynamics using an autoencoder neural network

Data-Driven Nonintrusive Model-Order Reduction for Aerodynamic Design Optimization

Wing design optimization and stall analysis with Co-flow Jet active control

A novel empirical model for vertical profiles of downburst horizontal wind speed

Nonintrusive Aerodynamic Shape Optimisation with a POD-DEIM Based Trust Region Method

Nonlinear Manifold Learning and Model Reduction for Transonic Flows

Aircraft parameter estimation using a stacked long short-term memory network and Levenberg-Marquardt method

Experimental design for a novel co-flow jet airfoil

Aerodynamic shape optimization of co-flow jet airfoil using a multi-island genetic algorithm

Analysis of the post-flutter aerothermoelastic characteristics of hypersonic skin panels using a CFD-based approach

Nonlinear reduced order modeling for nonlinear response simulation of panels via Large Eddy Simulation

Revisit of the variable stiffness method for aeroelastic computations with/without thermal effects based on computational fluid dynamics

A reduced-order model for gradient-based aerodynamic shape optimisation

Automated Mesh Deformation for Computer-Aided Design Models That Exhibit Boundary Topology Changes

Lock-in mechanism of flow over a low-Reynolds-number airfoil with morphing surface

Collaborators (4)

Hossein Malekmohamadi

Liang Sun

Simão Marques

Trevor Robinson

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