A test stand to investigate the rotor-stator interaction of a compressor stage is presented. This water channel allows to investigate the influence of wake depressions and choking to a stator cascade. Furthermore, adaptive blade systems are presented to affect the operating of stator under periodic unsteady flow conditions. The piezoelectric actuators are one of these adaptive blade systems. These can adjust the profile, so that the stator is more efficient than without.DFG, 200291049, SFB 1029: TurbIn - Signifikante Wirkungsgradsteigerung durch gezielte, interagierende Verbrennungs- und Strömungsinstationaritäten in Gasturbine
Active flow control is a technique to improve the fluid dynamics of an aerodynamic body utilizing an...
Investigation of the rotor-stator interactions of a reduced-scale model 0.19 ν= pump-turbine in gene...
Aircraft manufacturers and airlines require lightweight and compact but highly efficient engines in ...
At the Institute of Aeronautics and Astronautics of the Technische Universiẗat Berlin, an annular ca...
This thesis contributes to the field of active flow control of aerodynamically highly loaded compres...
In this dissertation results from a compressor cascade with periodic non-steady outflow conditions a...
Current methods for designing compressor blades in axial turbomachines assume that the flow through ...
Dieser Beitrag ist mit Zustimmung des Rechteinhabers aufgrund einer (DFG geförderten) Allianz- bzw. ...
With the goal of increasing the effciency of multi-stage compressors - particularly at part-load, an...
Closed-loop flow control was successfully demonstrated on the surface of stator vanes in NASA Glenn ...
Cogeneration of electric energy and heat as well as seasonal changes of the condenser pressure in lo...
This report documents an experimental and analytical study of the active stabilization of surge in a...
The objective of the ACONIT project is to design, manufacture and test actuators for flow control fo...
Virtual control surfaces for the optimization of steady and unsteady airloads on a compressor cascad...
ABSTRACT Recent research has revealed positive effects of unsteady flow on the development of profil...
Active flow control is a technique to improve the fluid dynamics of an aerodynamic body utilizing an...
Investigation of the rotor-stator interactions of a reduced-scale model 0.19 ν= pump-turbine in gene...
Aircraft manufacturers and airlines require lightweight and compact but highly efficient engines in ...
At the Institute of Aeronautics and Astronautics of the Technische Universiẗat Berlin, an annular ca...
This thesis contributes to the field of active flow control of aerodynamically highly loaded compres...
In this dissertation results from a compressor cascade with periodic non-steady outflow conditions a...
Current methods for designing compressor blades in axial turbomachines assume that the flow through ...
Dieser Beitrag ist mit Zustimmung des Rechteinhabers aufgrund einer (DFG geförderten) Allianz- bzw. ...
With the goal of increasing the effciency of multi-stage compressors - particularly at part-load, an...
Closed-loop flow control was successfully demonstrated on the surface of stator vanes in NASA Glenn ...
Cogeneration of electric energy and heat as well as seasonal changes of the condenser pressure in lo...
This report documents an experimental and analytical study of the active stabilization of surge in a...
The objective of the ACONIT project is to design, manufacture and test actuators for flow control fo...
Virtual control surfaces for the optimization of steady and unsteady airloads on a compressor cascad...
ABSTRACT Recent research has revealed positive effects of unsteady flow on the development of profil...
Active flow control is a technique to improve the fluid dynamics of an aerodynamic body utilizing an...
Investigation of the rotor-stator interactions of a reduced-scale model 0.19 ν= pump-turbine in gene...
Aircraft manufacturers and airlines require lightweight and compact but highly efficient engines in ...