Add to ORKGAn analysis was made of the flow trough a high-speed mixed-flow turbine based on axially symmetric conditions. The calculated weight flow was lower than that used in the two-dimensional design. The rotor could be redesigned to increase the weight flow and a flow and alleviate undesirable pressure gradients at the expense of increased rotor blade stresses
Modifying the original turbine by closing down the first-rotor throat area and shrouding the first a...
AbstractIn this paper, the design for the mixed flow compressor is based on the results of a S2 thro...
To support an active high-lift system for future civil aircraft small, electrically powered compress...
An analysis was made of the flow trough a high-speed mixed-flow turbine based on axially symmetric c...
A method of designing a new generation of highly loaded mixed flow turbines for turboc...
An investigation on new rotor blade designs conceived to produce higher exit relative kinetic energy...
[Objectives] The performance of a gas turbine engine can be determined by the performance of the com...
Flow through mixed flow compressor stage was evaluated theoretically to understand internal flow beh...
Abstract: The focus of this dissertation is the design of a mixed flow compressor stage with a press...
The performance of two mixed flow turbocharger turbine rotors is numerically investigated. Significa...
A turbine designed to power a supersonic compressor was investigated with four nozzle settings and o...
Special PaperPg. 139-148The results of a study on the aerodynamic performance of a high specific spe...
Special PaperPg. 139-148The results of a study on the aerodynamic performance of a high specific spe...
The quasi-three-dimensional method for the aerodynamic design of both stator and rotor blades is pre...
The aerodynamic performance of a high-work Mixed Flow Turbine (MFT) is computed and compared with ex...
Modifying the original turbine by closing down the first-rotor throat area and shrouding the first a...
AbstractIn this paper, the design for the mixed flow compressor is based on the results of a S2 thro...
To support an active high-lift system for future civil aircraft small, electrically powered compress...
An analysis was made of the flow trough a high-speed mixed-flow turbine based on axially symmetric c...
A method of designing a new generation of highly loaded mixed flow turbines for turboc...
An investigation on new rotor blade designs conceived to produce higher exit relative kinetic energy...
[Objectives] The performance of a gas turbine engine can be determined by the performance of the com...
Flow through mixed flow compressor stage was evaluated theoretically to understand internal flow beh...
Abstract: The focus of this dissertation is the design of a mixed flow compressor stage with a press...
The performance of two mixed flow turbocharger turbine rotors is numerically investigated. Significa...
A turbine designed to power a supersonic compressor was investigated with four nozzle settings and o...
Special PaperPg. 139-148The results of a study on the aerodynamic performance of a high specific spe...
Special PaperPg. 139-148The results of a study on the aerodynamic performance of a high specific spe...
The quasi-three-dimensional method for the aerodynamic design of both stator and rotor blades is pre...
The aerodynamic performance of a high-work Mixed Flow Turbine (MFT) is computed and compared with ex...
Modifying the original turbine by closing down the first-rotor throat area and shrouding the first a...
AbstractIn this paper, the design for the mixed flow compressor is based on the results of a S2 thro...
To support an active high-lift system for future civil aircraft small, electrically powered compress...