Numerical study of three-dimensional flow separation for a 6:1 ellipsoid
Author:
Affiliation:
1. Lockheed Martin Missiles & Space, Sunnyvale, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1999-172
Reference20 articles.
1. Experiments on an aerofoil at high angle of incidence in longitudinal oscillations
2. Detailed Investigation of the Three-Dimensional Separation About a 6:1 Prolate Spheroid
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1. Vortex shedding, flow separation, and drag coefficient in the flow past an ellipsoid of different aspect ratios at moderate Reynolds number;AIP Advances;2022-05-01
2. A DDES study of the flow past a prolate spheroid using a high-order U-MUSCL scheme;International Journal of Modern Physics B;2020-05-30
3. RANS models validation of the flow separation on a 6:1 prolate spheroid at angle of incidence;AIAA Scitech 2020 Forum;2020-01-05
4. Separated Flow Prediction Around a 6:1 Prolate Spheroid Using Reynolds Stress Models;Springer Tracts in Mechanical Engineering;2015
5. Evaluation of Hybrid RANS/LES Methods for Computing Flow over a Prolate Spheroid;Notes on Numerical Fluid Mechanics and Multidisciplinary Design;2014
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