Numerical Simulation of Transitional Flow Past a Wing Using Flux Reconstruction Method
Author:
Affiliation:
1. Yokohama National University, Yokohama 240-8501, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J054324
Reference39 articles.
1. GasterM. “The Structure and Behaviour of Laminar Separation Bubbles,” Aerodyne Research, Inc., Reports and Memoranda No. 3595, London, 1967.
2. High-order computational fluid dynamics tools for aircraft design
3. High-order CFD methods: current status and perspective
4. High-order methods for computational fluid dynamics: A brief review of compact differential formulations on unstructured grids
5. Advances in Bringing High-Order Methods to Practical Applications in Computational Fluid Dynamics
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. Efficient Implicit Method for a High-Order Flux Reconstruction Approach Using Modified Matrix-Free Defect Correction;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN;2022
2. Extension of the Flux Reconstruction Method to High-Reynolds Number RANS Simulations around High-Lift Devices;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2017
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