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Computation of Rarefied Gas Flows Around a NACA 0012 Airfoil

✍ Scribed by Fan, Jing; Boyd, Iain D.; Cai, Chun-Pei; Hennighausen, Konstantinos; Candler, Graham V.

Book ID
120544032
Publisher
American Institute of Aeronautics and Astronautics
Year
2001
Tongue
English
Weight
453 KB
Volume
39
Category
Article
ISSN
0001-1452

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πŸ“œ SIMILAR VOLUMES

Direct numerical simulation of flow sepa
Direct numerical simulation of flow separation around a NACA 0012 airfoil
✍ Hua Shan; Li Jiang; Chaoqun Liu πŸ“‚ Article πŸ“… 2005 πŸ› Elsevier Science 🌐 English βš– 687 KB

Direct numerical simulation (DNS) for the flow separation and transition around a NACA 0012 airfoil with an attack angle of 4Β°and Reynolds number of 10 5 based on free-stream velocity and chord length is presented. The details of the flow separation, detached shear layer, vortex shedding, breakdown