Periodic vortex shedding at the trailing edge of a turbine cascade has been investigated numerically for a subsonic and a transonic cascade flow. The numerical investigation was carried out by a finite volume multiblock code, solving the 2D compressible Reynolds-averaged Navier-Stokes equations on a
A method of computing transonic potential flows in turbine cascades
β Scribed by P.M. Byval'tsev; M.Ya. Ivanov
- Publisher
- Elsevier Science
- Year
- 1989
- Weight
- 713 KB
- Volume
- 29
- Category
- Article
- ISSN
- 0041-5553
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