Investigation of the compressible flow through the tip-section turbine blade cascade with supersonic inlet

Author:

Luxa Martin,Příhoda Jaromír,Šimurda David,Straka Petr,Synáč Jaroslav

Publisher

Springer Science and Business Media LLC

Subject

Condensed Matter Physics

Reference13 articles.

1. Luxa, M., Šimurda, D., Fort, J., Fürst, J., Šafarík, P., Synác, J., Rudas, B., (2015), Aerodynamic Investigation of Tip Section for Titanium Blade 54", Proceedings of the 11th European Conference on Turbomachinery Fluid Dynamics and Thermodynamics (ETC11), March 23–27, 2015, Madrid, Spain.

2. Parvizinia, M., Berlich, C., Truckenmüller, F., Stüer, H., (2004), Numerical and Experimental Investigations into the Aerodynamic Perfor-mance of a Supersonic Turbine Blade Profile, ASME Paper GT2004-53823, Atlanta, USA.

3. Shibata, T., Nakano, S., Ono, H., Morishita, K., Tani, Y., (2013), Linear Cascade Wind Tunnel Testing of Supersonic Inflow and Outflow Turbine Blades, Transactions of JSME, Series B, Vol. 79, No.806, pp. 2120–2133

4. Senoo, S., Asai, K., Kurosawa, A., Lee, G., (2013), Titanium 50-inch and 60-inch Last-stage Blades for Steam Turbines, Hitachi Review, Vol. 62, No. 1

5. Šimurda, D., Luxa, M., Šafarík, P., Synác, J. and Rudas, B., (2014), Measurements on Supersonic Turbine Cascades-Methodical Approach, Proceedings of the XXII Symposium on Measuring Techniques in Turbomachinery, Lyon, France.

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