Add to ORKG<p>In this work the interaction of flutter-a self-excited self-sustained aeroelastic vibration phenomenon-with wake excitation is investigated using a harmonic balance frequency domain CFD code to solve the 2D inviscid Euler equations for a rotor in choke flutter operation. The wake deficit and the blade-motion amplitude (torsion) are varied.</p>Thesi
The ERATO rotor blade is assessed for flutter stability in hover. For the aeroelastic analyses, the ...
Aeroelastic phenomena in turbomachinery are one of the most challenging problems to model using comp...
State-of-the-art prediction of the aeroelastic stability of cascades in axial-flow turbomachines is ...
Blades of turbomachine are important components to produce power like turbines or pressure compresso...
Modern turbomachines are designed towards thinner, lighter and highly loaded blades. This gives rise...
During the design of the compressor and turbine stages oftoday's aeroengines aerodynamically induced...
The paper presents a 3D numerical simulation of flow in a blade cascade, whose geometry models the t...
A parametric study of the unstalled flutter stability character- istics of compressor and turbine ca...
Effects of frequency mistuning on cascade flutter are studied using a computational method with coup...
The onset and spread of flutter in a turbine blade cascade are numerically studied. Due to the appl...
In recent years coupled fluid-structure problems have appeared. The computational method used to sol...
Flutter and forced response analyses for a cascade of blades in subsonic and transonic flow is prese...
ABSTRACT A three-dimensional nonlinear time-marching method and numerical analysis for aeroelastic b...
This contribution is connected with the paper on the previous conference, where the origin and prope...
AbstractA coupled fluid-structure method is developed for flutter analysis of blade vibrations in tu...
The ERATO rotor blade is assessed for flutter stability in hover. For the aeroelastic analyses, the ...
Aeroelastic phenomena in turbomachinery are one of the most challenging problems to model using comp...
State-of-the-art prediction of the aeroelastic stability of cascades in axial-flow turbomachines is ...
Blades of turbomachine are important components to produce power like turbines or pressure compresso...
Modern turbomachines are designed towards thinner, lighter and highly loaded blades. This gives rise...
During the design of the compressor and turbine stages oftoday's aeroengines aerodynamically induced...
The paper presents a 3D numerical simulation of flow in a blade cascade, whose geometry models the t...
A parametric study of the unstalled flutter stability character- istics of compressor and turbine ca...
Effects of frequency mistuning on cascade flutter are studied using a computational method with coup...
The onset and spread of flutter in a turbine blade cascade are numerically studied. Due to the appl...
In recent years coupled fluid-structure problems have appeared. The computational method used to sol...
Flutter and forced response analyses for a cascade of blades in subsonic and transonic flow is prese...
ABSTRACT A three-dimensional nonlinear time-marching method and numerical analysis for aeroelastic b...
This contribution is connected with the paper on the previous conference, where the origin and prope...
AbstractA coupled fluid-structure method is developed for flutter analysis of blade vibrations in tu...
The ERATO rotor blade is assessed for flutter stability in hover. For the aeroelastic analyses, the ...
Aeroelastic phenomena in turbomachinery are one of the most challenging problems to model using comp...
State-of-the-art prediction of the aeroelastic stability of cascades in axial-flow turbomachines is ...