An improved nonlinear reduced-order modeling for transonic aeroelastic systems-Reference-Cited by-同舟云学术

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An improved nonlinear reduced-order modeling for transonic aeroelastic systems

Published:2020-04 Issue: Volume:94 Page:102926
ISSN:0889-9746
Container-title:Journal of Fluids and Structures
language:en
Short-container-title:Journal of Fluids and Structures

Author:

Yang Zhijun,Huang Rui,Liu Haojie,Zhao Yonghui,Hu Haiyan

Funder

National Natural Science Foundation of China

Nanjing University of Aeronautics and astronautics, China

Equipment Pre-Research Foundation, China

Publisher

Elsevier BV

Subject

Mechanical Engineering

Reference46 articles.

1. Application of multi-input Volterra theory to nonlinear multi-degree-of-freedom aerodynamic systems;Balajewicz;AIAA J.,2010

2. Review of unsteady transonic aerodynamics: theory and applications;Bendiksen;Prog. Aerosp. Sci.,2011

3. Reduced-order modelling of limit-cycle oscillation for aeroelastic systems;Beran;J. Fluids Struct.,2004

4. Nonlinear transonic flutter analysis;Borland;AIAA J.,1982

5. Limit cycle oscillation characteristics of fighter aircraft;Bunton;J. Aircr.,2000

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1. An Effective Arbitrary Lagrangian-Eulerian-Lattice Boltzmann Flux Solver Integrated with the Mode Superposition Method for Flutter Prediction;Applied Sciences;2024-05-05

2. Transonic Aerodynamic–Structural Coupling Characteristics Predicted by Nonlinear Data-Driven Modeling Approach;AIAA Journal;2024-03

3. Asymptotic stability of a nonlinear energy harvester with mass disturbance undergoing Markovian jump;Applied Mathematical Modelling;2024-03

4. Optimisation of initial velocity distribution of jets for entrainment and diffusion control using deep reinforcement learning;International Journal of Heat and Mass Transfer;2024-01

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