Xiaomin An

Northwestern Polytechnical University — China

Engineering · Physical Sciences

6h-index129citations25works0.02yr avg
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Research Topics

Computational Fluid Dynamics and Aerodynamics(12), Vibration and Dynamic Analysis(8), Fluid Dynamics and Vibration Analysis(7), Composite Structure Analysis and Optimization(4), Aeroelasticity and Vibration Control(4)

Publications25 total

A new data-driven model for predicting the nonlinear aeroelastic behavior of panels
Thin-Walled Structures·2025
Analysis of nonlinear aeroelastic response of curved panels under shock impingements
Journal of Fluids and Structures·2021· 13 cited
Numerical study on the trajectory of a long-range flexible rocket with large slenderness ratio
Aerospace Science and Technology·2021· 4 cited
Nonlinear reduced order modeling for nonlinear response simulation of panels via Large Eddy Simulation
Journal of Sound and Vibration·2021· 2 citedOpen Access
Aero-structural optimization of supersonic wing under thermal environment using adjoint-based optimization algorithm
Structural and Multidisciplinary Optimization·2021· 10 cited
Index
2020
Chapter 3 Numerical method for nonlinear structural response computation with geometric nonlinearity
2020
Chapter 2 Unsteady CFD technology
2020
Modern Computational Aeroelasticity
2020· 6 cited
Study of aeroelastic REsponse of cylindrical composite panels in A high-speed flow
International Journal of Modern Physics B·2020· 1 cited
Numerical simulation of nonlinear aeroelastic behaviors of composite panels in transonic flow
Journal of Sound and Vibration·2019· 10 cited
A Highly Efficient Grid Deformation Strategy Based on Proper Orthogonal Decomposition
Lecture notes in electrical engineering·2019
Aerodynamic and Aeroelastic Analysis of Flying Wing with Split Drag-Rudder
Lecture notes in electrical engineering·2019
Nonlinear flutter analysis of composite panels
Modern Physics Letters B·2018· 6 cited
Nonlinear aeroelastic analysis of curved laminated composite panels
Composite Structures·2017· 20 cited
Post-flutter response of a flexible cantilever plate in low subsonic flows
International Journal of Non-Linear Mechanics·2017· 10 cited
Nonlinear Panel Flutter Analysis Based on an ImprovedCFD/CSD Coupled Procedure
Computer Modeling in Engineering & Sciences·2014· 5 citedOpen Access
Limit Cycle Oscillation and Nonlinear Aeroelastic Response Analysis Using Corotational Theory
51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition·2013
A Mesh Deformation Method for Aeroelastic Simulation
2010
Improved Algorithm for CFD/CSD Coupled System Design and Calculation
Transaction of Nanjing University of Aeronautics and Astronautics·2010· 2 cited
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Frequent Co-authors

Min Xu(11), Guangning Li(4), Wei Xu(3), Bin Deng(2), Wei Sun(2), Dan Xie(2), Min Xu(2), Yabin Wang(2), Shutian Liu(1), Haipeng Jia(1), Boo Cheong Khoo(1), Yongdong Cui(1), Jiayue Feng(1), Youwen Qu(1), Baiyi Qi(1), Tao Chen(1), Jingrui Guo(1), Yi Li(1), Yan Wang(1), Min Xu(1)