Computation of flow around a circular cylinder in a supercritical regime
Author:
Affiliation:
1. Tokyo, University, Japan
2. National Aerospace Laboratory, Tokyo, Japan
3. NASA, Ames Research Center, Moffett Field, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1985-1660
Reference22 articles.
Cited by 6 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. Investigation of drag reduction on a two-dimensional circular cylinder by ejecting a jet from the rear stagnation region;36th AIAA Aerospace Sciences Meeting and Exhibit;1998-01-12
2. Vortex-shedding Flow Predictions with Eddy-viscosity Models;Engineering Turbulence Modelling and Experiments;1993
3. Flow Simulation on Supercomputers and Its Visualization;Turbulence and Molecular Processes in Combustion;1993
4. Finite-element analysis of high Reynolds number flow past a circular cylinder;Journal of Computational and Applied Mathematics;1991-12
5. A vortex panel analysis of circular-arc bluff-bodies in unsteady flow;10th Aerodynamic Decelerator Conference;1989-04-18
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