An experimental investigation of the dissipation mechanisms in the suction side boundary layer of a turbine blade

Author:

Satta Francesca,Simoni Daniele,Ubaldi Marina,Zunino Pietro

Publisher

Springer Science and Business Media LLC

Subject

Condensed Matter Physics

Reference20 articles.

1. Denton, J.D.: Loss Mechanisms in Turbomachines, Journal of Turbomachinery, vol. 115, pp. 621–656, (1993).

2. Griffin, P.C., Davies, M.R.D., O’Donnell, F.K., Walsh, E.: The Effect of Reynolds Number, Compressibility and Free Stream Turbulence on Profile Entropy Generation Rate, ASME Paper No. GT-2002-30330, (2002).

3. Moore, J., Shaffer, D.M., Moore, J.G.: Reynolds Stresses and Dissipation Mechanisms Downstream of a Turbine Cascade, ASME Journal of Turbomachinery, vol. 109, pp. 258–267, (1986).

4. Canepa, E., Cattanei, A., Pittaluga, F., Ubaldi, M., Zunino, P.: “Transitional boundary layer on the suction side of a turbine blade at different Reynolds numbers”, 5th European Conference on Turbomachinery, Praha, (2003).

5. Ubaldi, M., Zunino, P., Campora, U., Ghiglione, A.: Detailed Velocity and Turbulence Measurements of the Profile Boundary Layer in a Large Scale Turbine Cascade, ASME Paper No. 96-GT-42, (1996).

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