Hybrid Finite-Volume Reduced-Order Model Method for Nonlinear Aeroelastic Modeling-Reference-Cited by-同舟云学术

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Hybrid Finite-Volume Reduced-Order Model Method for Nonlinear Aeroelastic Modeling

Published:2014-11 Issue:6 Volume:51 Page:1805-1812
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Mowat Andrew G. B.¹,Malan Arnaud G.¹,van Zyl Louw H.²,Meyer Josua P.³

Affiliation:

1. Department of Mechanical Engineering, University of Cape Town, Cape Town 7701, South Africa

2. Defence Peace Safety and Security, Council for Scientific and Industrial Research, Pretoria 0001, South Africa

3. Department of Mechanical and Aeronautical Engineering, University of Pretoria, Pretoria 0028, South Africa

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C032524

Reference49 articles.

1. A review of numerical fluids/structures interface methods for computations using high-fidelity equations

2. Numerical model of unsteady subsonic aeroelastic behavior

3. WING FLUTTER BOUNDARY PREDICTION USING UNSTEADY EULER AERODYNAMIC METHOD

4. Mixed explicit/implicit time integration of coupled aeroelastic problems: Three-field formulation, geometric conservation and distributed solution

5. Partitioned procedures for the transient solution of coupled aroelastic problems Part I: Model problem, theory and two-dimensional application

Cited by 5 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. A provably stable and high-order accurate finite difference approximation for the incompressible boundary layer equations;Computers & Fluids;2023-12

2. Aeroelastic Reduced Order Model: Kriging-Corrected Potential Flow;Journal of Aircraft;2020-05

3. Hybrid Computational-Fluid-Dynamics Platformto Investigate Aircraft Trailing Vortices;Journal of Aircraft;2019-01

4. High Fidelity Gust Simulations Over a Supercritical Airfoil;2018 Applied Aerodynamics Conference;2018-06-24

5. A Kriging Based Corrected Potential Flow ROM for Gust Load Calculations;2018 Applied Aerodynamics Conference;2018-06-24

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