AbstractTo design more efficient film cooling geometries for gas turbines, non-intrusive measurements of the flow temperature, velocity and derived quantities like the turbulent heat flux are needed in well-defined, generic flow configurations. With this aim we have applied thermographic particle image velocimetry (thermographic PIV) to investigate the flow emanating from angled and trenched cooling holes in a closed-loop optically-accessible wind tunnel facility. BAM:Eu2+ thermographic phosphor particles were seeded into the flow as a tracer. A pulsed high-speed UV laser was used to excite the particles and the luminescence was detected using two high-speed cameras to determine the temperature field by a two-colour ratiometric approach. Th...
Experiments to measure the temperature field downstream of simulated leading-edge-region film-coolin...
Cooling combustor chambers for gas turbine engines is challenging, given the complex flow and therma...
The benefits of different film cooling geometries are typically assessed in terms of their time aver...
During film-hole cooling, relatively cold air is extracted from the compressor of a gas turbine engi...
ABSTRACT The turbulent flow field of a film cooling flow is investigated using the particle-image ve...
Particle image velocimetry and particle scattering measurements are taken over a flat multi-row film...
Film-cooling is one of the most prevalent cooling technologies that is used for gas turbine airfoil ...
The research presented in this paper strives to exploit the benefits of near-wall measurement capabi...
This paper presents flow visualisation experiments for a novel film-cooling hole, the converging s...
An experimental study was conducted to investigate both the aerodynamic and the thermal behavior of ...
Film cooling is crucial in the field of gas turbines to protect the blade surfaces from the hot comb...
Film cooling in modern gas turbine engines uses coolant from the compressor to protect the surface o...
Thermal convective air flows are of great relevance in fundamental studies and technical application...
The benefits of different film cooling geometries are typically assessed in terms of their time-aver...
Film cooling is vital for the cooling of the blades and vanes in the high temperature environment of...
Experiments to measure the temperature field downstream of simulated leading-edge-region film-coolin...
Cooling combustor chambers for gas turbine engines is challenging, given the complex flow and therma...
The benefits of different film cooling geometries are typically assessed in terms of their time aver...
During film-hole cooling, relatively cold air is extracted from the compressor of a gas turbine engi...
ABSTRACT The turbulent flow field of a film cooling flow is investigated using the particle-image ve...
Particle image velocimetry and particle scattering measurements are taken over a flat multi-row film...
Film-cooling is one of the most prevalent cooling technologies that is used for gas turbine airfoil ...
The research presented in this paper strives to exploit the benefits of near-wall measurement capabi...
This paper presents flow visualisation experiments for a novel film-cooling hole, the converging s...
An experimental study was conducted to investigate both the aerodynamic and the thermal behavior of ...
Film cooling is crucial in the field of gas turbines to protect the blade surfaces from the hot comb...
Film cooling in modern gas turbine engines uses coolant from the compressor to protect the surface o...
Thermal convective air flows are of great relevance in fundamental studies and technical application...
The benefits of different film cooling geometries are typically assessed in terms of their time-aver...
Film cooling is vital for the cooling of the blades and vanes in the high temperature environment of...
Experiments to measure the temperature field downstream of simulated leading-edge-region film-coolin...
Cooling combustor chambers for gas turbine engines is challenging, given the complex flow and therma...
The benefits of different film cooling geometries are typically assessed in terms of their time aver...