Improved Nonlinear Analysis of a Propeller Blade Based on Hyper-Reduction-Reference-Cited by-同舟云学术

Improved Nonlinear Analysis of a Propeller Blade Based on Hyper-Reduction

Published:2021-12-22 Issue: Volume: Page:1-14
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Kim Yongse¹,Kang Seung-Hoon¹,Cho Haeseong²,Shin SangJoon¹^ORCID

Affiliation:

1. Seoul National University, Seoul 08826, Republic of Korea

2. Jeonbuk National University, Jeollabuk-do 54896, Republic of Korea

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J060742

Reference41 articles.

1. Reduced order modeling for nonlinear structural analysis using Gaussian process regression

2. ORBIT: Optimization by Radial Basis Function Interpolation in Trust-Regions

3. Kriging Models for Global Approximation in Simulation-Based Multidisciplinary Design Optimization

4. RizziS. A.MuravyovA. A. “Improved Equivalent Linearization Implementations Using Nonlinear Stiffness Evaluation,” NASA TM-2001-210838, L-18068, NAS 1.15:210838, 2001.

5. Reduced Order Models for Nonlinear Dynamic Analysis With Application to a Fan Blade

Cited by 12 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. Feasible model-order reduction approach for analysis of composite rotor blades based on geometrically exact beam formulation;Aerospace Science and Technology;2024-09

2. Comparison of Hyper-Reduction Methods Combined With POD: Model Order Reduction of a Squirrel Cage Induction Machine in Nonlinear Case;IEEE Transactions on Magnetics;2024-06

3. Improved multi-body contact analysis based on the hyper-reduction approach;AIAA SCITECH 2024 Forum;2024-01-04

4. Efficient implementation on accuracy improvement of the two-dimensional node-to-segment contact approach for explicit dynamic analysis;Computational Mechanics;2023-12-19

5. Model Reduction of Isogeometric Shell Structures For Large-Scale Design Optimization;AIAA AVIATION 2023 Forum;2023-06-08