Add to ORKGThe paper deals with selected phenomena present in a blade cascade flow field. The presented research was performed on prismatic blade cascades composed mostly of the tip and root sections of the last stage rotor blade of a large output steam turbine. The unstarted supersonic flow on the cascade inlet, the separation of the flow and the swirl line behind the trailing edge have been identified as the possible sources of the unsteady force effects
So far no theory of the Reaction Turbine has as yet been investigated which is capable of clarifying...
A blade cascade allowing free pitch movement of five blades was developed in Institute of Thermomech...
Present day military aero-gas turbines demand higher stage loadings for turbines so as to meet the ...
The paper deals with selected phenomena present in a blade cascade flow field. The presented researc...
The paper describes the results of a numerical and experimental research program addressing the aero...
The motivation of this paper is the continual development of the blades for the last stage of the st...
Experimental investigations have been carried out on a steam turbine rotor tip linear cascade to det...
A two-dimensional section of the last stage of a steam turbine blade has been investigated experimen...
One method aircraft engine manufactures use to minimize engine cost and weight is to reduce the numb...
The paper is focused on aerodynamic characteristics of the tip section of a steam turbine last stage...
Technology Agency of the Czech Republic under the National Centre for Power Engineering TH1000072. I...
The paper deals with experimental results of high-speed aerodynamic research on a blade cascade. The...
Long term strategic changes in power generation approaches will require more flexibility for large p...
the research project of Czech science foundation No. 20-26779S “Study of dynamic stall flutter insta...
This thesis describes the design of a water table analog to simulate and study the parameters associ...
So far no theory of the Reaction Turbine has as yet been investigated which is capable of clarifying...
A blade cascade allowing free pitch movement of five blades was developed in Institute of Thermomech...
Present day military aero-gas turbines demand higher stage loadings for turbines so as to meet the ...
The paper deals with selected phenomena present in a blade cascade flow field. The presented researc...
The paper describes the results of a numerical and experimental research program addressing the aero...
The motivation of this paper is the continual development of the blades for the last stage of the st...
Experimental investigations have been carried out on a steam turbine rotor tip linear cascade to det...
A two-dimensional section of the last stage of a steam turbine blade has been investigated experimen...
One method aircraft engine manufactures use to minimize engine cost and weight is to reduce the numb...
The paper is focused on aerodynamic characteristics of the tip section of a steam turbine last stage...
Technology Agency of the Czech Republic under the National Centre for Power Engineering TH1000072. I...
The paper deals with experimental results of high-speed aerodynamic research on a blade cascade. The...
Long term strategic changes in power generation approaches will require more flexibility for large p...
the research project of Czech science foundation No. 20-26779S “Study of dynamic stall flutter insta...
This thesis describes the design of a water table analog to simulate and study the parameters associ...
So far no theory of the Reaction Turbine has as yet been investigated which is capable of clarifying...
A blade cascade allowing free pitch movement of five blades was developed in Institute of Thermomech...
Present day military aero-gas turbines demand higher stage loadings for turbines so as to meet the ...