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
β¦ LIBER β¦
Numerical simulation of thrust generating flow past a pitching airfoil
β Scribed by Sunetra Sarkar; Kartik Venkatraman
- Publisher
- Elsevier Science
- Year
- 2006
- Tongue
- English
- Weight
- 814 KB
- Volume
- 35
- Category
- Article
- ISSN
- 0045-7930
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