Direct numerical simulation (DNS) for the flow separation and transition around a NACA 0012 airfoil with an attack angle of 4°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
✦ LIBER ✦
Numerical investigation of separated flow around a bent-nose biconic
✍ Scribed by Norio Arai; Syuji Sakaguchi; Yasuhiro Wada; Satoru Ogawa
- Publisher
- Elsevier Science
- Year
- 1991
- Tongue
- English
- Weight
- 664 KB
- Volume
- 35
- Category
- Article
- ISSN
- 0377-0427
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The occurrence of separated ¯ow in sharply curving river bends, and the associated deposition of ®ne-grained sediment, is widely recognized, but the factors controlling the existence and extent of separated ¯ow have not been clearly identi®ed. A three-dimensional, ®xed lid computational ¯uid dynamic