Add to ORKGThis work was supported by the GA CR project No. 20-26779S Study of dynamic stall flutter instabilities and their consequences in turbomachinery application using mathematical, nu- merical and experimental methods. Validation would not be possible without the AVL Excite software, which is available in the framework of the University Partnership program of AVL List GmbH and whose usage is greatly acknowledge
The present study aims to investigate the synchronization characteristics of a pitch–plunge aeroelas...
Current trends in turbomachinery design significantly reduce the mass ratio of structure to air, mak...
Turbomachinery components are exposed to unsteady aero- dynamic loads which must be considered duri...
This work was supported by the GA CR project No. 20-26779S Study of dynamic stall flutter instabili...
<p>One of the grand challenges faced by industry is the accurate prediction of unsteady aerodynamics...
International audienceThe mechanism underlying the lock-in of frequencies in flow-induced vibrations...
<p>This research presents the detailed investigation of coupled-mode flutter and non-synchronous vib...
The frequency lock-in during the nonlinear vibration of a turbomachinery blade is modeled using a sp...
This work was supported by the research project of the Czech Science Foundation Study of dynamic st...
The present study aims to investigate the lock-in phenomena due to the coupling of the pitch and the...
In the field of turbomachinery mechanical designs strive for increased efficiency and lighter engine...
To save resources and reduce emissions, it is crucial to reduce weight of aircraft engines and furth...
Prediction of flutter in shrouded turbomachinery cascades is difficult due to i) coupling of aerodyn...
Non-synchronous vibrations arising near the stall boundary of compressors are a recurring and potent...
This thesis describes the development and application of a methodology for modelling fluid-structure...
The present study aims to investigate the synchronization characteristics of a pitch–plunge aeroelas...
Current trends in turbomachinery design significantly reduce the mass ratio of structure to air, mak...
Turbomachinery components are exposed to unsteady aero- dynamic loads which must be considered duri...
This work was supported by the GA CR project No. 20-26779S Study of dynamic stall flutter instabili...
<p>One of the grand challenges faced by industry is the accurate prediction of unsteady aerodynamics...
International audienceThe mechanism underlying the lock-in of frequencies in flow-induced vibrations...
<p>This research presents the detailed investigation of coupled-mode flutter and non-synchronous vib...
The frequency lock-in during the nonlinear vibration of a turbomachinery blade is modeled using a sp...
This work was supported by the research project of the Czech Science Foundation Study of dynamic st...
The present study aims to investigate the lock-in phenomena due to the coupling of the pitch and the...
In the field of turbomachinery mechanical designs strive for increased efficiency and lighter engine...
To save resources and reduce emissions, it is crucial to reduce weight of aircraft engines and furth...
Prediction of flutter in shrouded turbomachinery cascades is difficult due to i) coupling of aerodyn...
Non-synchronous vibrations arising near the stall boundary of compressors are a recurring and potent...
This thesis describes the development and application of a methodology for modelling fluid-structure...
The present study aims to investigate the synchronization characteristics of a pitch–plunge aeroelas...
Current trends in turbomachinery design significantly reduce the mass ratio of structure to air, mak...
Turbomachinery components are exposed to unsteady aero- dynamic loads which must be considered duri...