Transition on turbine blades is an important factor in the determination of eventual flow separation and engine performance. The phenomenon is strongly affected by unsteady flow conditions (wake passing). It is likely that some physics of unsteadiness should be included in advanced models, but it is unclear which properties would best embody this information. In this paper, we use a GEAE experimental database in unsteady transition to test some tools of spot identification, tracking and characterization. In this preliminary study, we identify some parameters that appear to be insensitive to wake passing effects, such as convection speed, and others more likely to require unsteady modeling. The main findings are that wavelet duration can be ...
Within a European project a high-pressure turbine stage was investigated at DLR, Goettingen. The inv...
The flow around a gas turbine blade is inherently three-dimensional and based on the Re-number and t...
The present paper is the second part of a two-part paper focused on the design and the analysis of a...
Experimental work at the University of Oxford Osney Lab has demonstrated characteristics of the late...
In turbomachinery, a considerable proportion of the blade surface area can be covered transitional b...
Experimental data describing laminar separation bubbles developing under strong adverse pressure gra...
Large loading events on wind turbine rotor blades are often associated with transient bursts of cohe...
The paper analyzes the unsteady interaction between an impinging wake and the suction side boundary ...
The study of wind turbine blade aerodynamics during full operation has only recently received attent...
An investigation into the unsteady losses in a high pressure turbine stage has been performed experi...
In this paper the unsteady flow field of a highly loaded turbine rotor blade at different transonic ...
Wind turbine power production and its variability are affected by unsteady, turbulent structures tha...
An investigation into the unsteady losses in a high pressure turbine stage has been performed experi...
The development of streamwise-orientated disturbances at transition onset for zero-pressure gradient...
This thesis documents an experimental and computational study of the unsteady flow around oscillatin...
Within a European project a high-pressure turbine stage was investigated at DLR, Goettingen. The inv...
The flow around a gas turbine blade is inherently three-dimensional and based on the Re-number and t...
The present paper is the second part of a two-part paper focused on the design and the analysis of a...
Experimental work at the University of Oxford Osney Lab has demonstrated characteristics of the late...
In turbomachinery, a considerable proportion of the blade surface area can be covered transitional b...
Experimental data describing laminar separation bubbles developing under strong adverse pressure gra...
Large loading events on wind turbine rotor blades are often associated with transient bursts of cohe...
The paper analyzes the unsteady interaction between an impinging wake and the suction side boundary ...
The study of wind turbine blade aerodynamics during full operation has only recently received attent...
An investigation into the unsteady losses in a high pressure turbine stage has been performed experi...
In this paper the unsteady flow field of a highly loaded turbine rotor blade at different transonic ...
Wind turbine power production and its variability are affected by unsteady, turbulent structures tha...
An investigation into the unsteady losses in a high pressure turbine stage has been performed experi...
The development of streamwise-orientated disturbances at transition onset for zero-pressure gradient...
This thesis documents an experimental and computational study of the unsteady flow around oscillatin...
Within a European project a high-pressure turbine stage was investigated at DLR, Goettingen. The inv...
The flow around a gas turbine blade is inherently three-dimensional and based on the Re-number and t...
The present paper is the second part of a two-part paper focused on the design and the analysis of a...