## Abstract A thin shear layer moving from the trailing edge of a twoโdimensional aerofoil section downstream can be interpreted as a curve of discontinuity for the tangential velocity and may be approximated by a vortex sheet in inviscid, incompressible fluid flow. It is well known that vortex she
โฆ LIBER โฆ
Spiral vortex solution of Birkhoff-Rott equation
โ Scribed by T. Kambe
- Publisher
- Elsevier Science
- Year
- 1989
- Tongue
- English
- Weight
- 919 KB
- Volume
- 37
- Category
- Article
- ISSN
- 0167-2789
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