Model Reduction of Hypersonic Aerodynamics with residual minimization techniques
Author:
Affiliation:
1. Sandia National Laboratories California
2. NexGen Analytics
3. Sandia National Laboratories
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2022-1247
Reference58 articles.
1. Slotnick, J., Khodadoust, A., Alonso, J., Darmofal, D., Gropp, W., Lurie, E., and Mavriplis, D. “CFD vision 2030 study: a path to revolutionary computational aerosciences,” Tech. Rep. NASA/CR-2014-218178, NASA, March 2014.
2. A review on design of experiments and surrogate models in aircraft real-time and many-query aerodynamic analyses
3. POD-based Aeroelastic Analysis of a Complete F-16 Configuration: ROM Adaptation and Demonstration
4. Interpolation Method for Adapting Reduced-Order Models and Application to Aeroelasticity
5. Efficient non-linear model reduction via a least-squares Petrov-Galerkin projection and compressive tensor approximations
Cited by 2 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. Projection-based Reduced-Order Models with Hyperreduction for Finite Element Simulations of Thermal Protection Systems;AIAA AVIATION 2023 Forum;2023-06-08
2. Residual minimization formulations for model reduction of steady hypersonic flow;AIAA AVIATION 2023 Forum;2023-06-08
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