An investigation of secondary-flow loss cores originating in turbine nozzle blade passages was conducted by means of flow visualization studies and detailed flow measurements. The degree of which blade surface velocity profiles affect the magnitude and concentration of loss cores was investigated by comparing three nozzle blade configurations.NACA TN No. 2989."August 1953."Includes bibliographical references.An investigation of secondary-flow loss cores originating in turbine nozzle blade passages was conducted by means of flow visualization studies and detailed flow measurements. The degree of which blade surface velocity profiles affect the magnitude and concentration of loss cores was investigated by comparing three nozzle blade configur...
Thesis (Sc.D.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1979.MICROFI...
The experimental performance of turbine nozzle blades designed for a constant discharge angle was in...
Plane turbine cascades are used to improve the capability to predict aerodynamic loss, loading, and ...
An investigation was made of losses and secondary flows in three different turbine nozzle configurat...
An investigation of secondary-flow loss patterns originating in three sets of turbine nozzle blade p...
At one flow condition investigated, the radial transport of low-momentum fluid in the blade wake and...
In order to increase understanding of the origin of losses in a turbine, the secondary-flow componen...
An investigation of secondary-flow loss patterns originating in three sets of turbine nozzle blade p...
Still and motion pictures were made of boundary-layer and wake secondary-flow phenomena visualized b...
A primary objective of turbine research is to obtain information that will aid in the design of gas ...
Still and motion pictures were made of boundary-layer and wake secondary-flow phenomena visualized b...
At the request of the Junkers Aircraft and Engine Construction Company, Engine Division, Dessau Main...
Detailed circumferential and radial surveys of total pressure and t o t a l temperature w e r e mad...
In turbomachines, secondary flows (or endwall flows) typically originate at the junction between end...
article image velocimetry measurements have been carried out in a low-pressure turbine cascade opera...
Thesis (Sc.D.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1979.MICROFI...
The experimental performance of turbine nozzle blades designed for a constant discharge angle was in...
Plane turbine cascades are used to improve the capability to predict aerodynamic loss, loading, and ...
An investigation was made of losses and secondary flows in three different turbine nozzle configurat...
An investigation of secondary-flow loss patterns originating in three sets of turbine nozzle blade p...
At one flow condition investigated, the radial transport of low-momentum fluid in the blade wake and...
In order to increase understanding of the origin of losses in a turbine, the secondary-flow componen...
An investigation of secondary-flow loss patterns originating in three sets of turbine nozzle blade p...
Still and motion pictures were made of boundary-layer and wake secondary-flow phenomena visualized b...
A primary objective of turbine research is to obtain information that will aid in the design of gas ...
Still and motion pictures were made of boundary-layer and wake secondary-flow phenomena visualized b...
At the request of the Junkers Aircraft and Engine Construction Company, Engine Division, Dessau Main...
Detailed circumferential and radial surveys of total pressure and t o t a l temperature w e r e mad...
In turbomachines, secondary flows (or endwall flows) typically originate at the junction between end...
article image velocimetry measurements have been carried out in a low-pressure turbine cascade opera...
Thesis (Sc.D.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1979.MICROFI...
The experimental performance of turbine nozzle blades designed for a constant discharge angle was in...
Plane turbine cascades are used to improve the capability to predict aerodynamic loss, loading, and ...