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Influence of air cooling and air-jet vortex generator on flow structure in turbine passage

Szwaba R., Flaszyński P., Szumski J. A., Doerffer P.

TASK Quarterly : scientific bulletin of Academic Computer Centre in Gdansk

2015

Vol. 19, No 2

153--166

The paper concerns the experimental investigations and numerical simulations of a high loaded model of a turbine blade. An increase in the blade load leads to enlargement of a local supersonic zone terminated by a shock wave on the suction side. The Mach number upstream of the shock reaches up to 1.6. The interaction of the shock wave with a boundary layer at such a high Mach number leads to a strong separation. Streamwise vortices generated by air-jets were used for the interaction control. The work presents the experimental and numerical results of the application of an air-jets vortex generator on the suction side of cooled turbine blades. Very interesting results were obtained in the context of the air cooling and air-jet vortex generator influence on the flow structure in the turbine passage.

Application of the pressure sensitive paint method for transonic flow measurements

Szumski J. A., Doerffer P.

Turbulence : international journal

2005

Vol. 11

55-63

Traditional measurements of the pressure distribution are conducted with use of pressure taps. Those pressure taps require model surface to be drilled through. In case of such intrusive pressure measurements the instrumentation and model mounting become a problem, especially in case of rotating compressor or turbine blades. The new optical method based on pressure (oxygen concentration) sensitive paints allow to obtain a continuous pressure distribution on the model surface in essentially non-intrusive way. The PSP technology helps understanding of the flow around the model and provides quantitative flow data for further processing. PSP method treated in this paper proved to be a very good solution for complex flows. The scope of this paper is to present the basics of the PSP method. It covers only the basic equations, general idea of the method, typical system set up and some of the approaches to PSP paint application. Typical PSP system is explained as well as the formulation of the PSP paint. The physical phenomena of the excitation, emission and oxygen quenching is explained. Deployment of the system at IFFM PAS is in the final stage, and preliminary calibration results are available. At the end of this paper the IFFM PAS plans for future, current PSP development challenges, actions to be taken, and some of the expected results are discussed.