The continuing rise in turbine entry temperatures has necessitated the development of ever-more advanced cooling techniques. Effusion cooling is an example of such a system and is characterised by a high density of film cooling holes that operate at low blowing ratios, thereby achieving high overall cooling effectiveness. This paper presents both an experimental and computational investigation into the cooling performance of effusion systems. Two flat-plate geometries (with primary hole pitches of 3.0D and 5.75D) are experimentally investigated via a pressure sensitive paint technique yielding high resolution film effectiveness distributions via heat-mass transfer analogy. A computational fluid dynamics (CFD) scalar tracking method was used...
The continuous drive for ever higher turbine entry temperatures is leading to considerable interest ...
Transpiration cooling represents the pinnacle of turbine cooling and is characterized by an intrinsi...
The present study aims to investigate the effectiveness of effusion film cooling on an adiabatic fla...
The continuing rise in turbine entry temperatures has necessitated the development of ever-more adva...
The continuing rise in turbine entry temperatures has necessitated the development of evermore advan...
The continuing rise in turbine entry temperatures has necessitated the development of evermore advan...
The continuing rise in turbine entry temperatures has necessitated the development of evermore advan...
This thesis presents CFD predictions of gas turbine film and effusion cooling. The dearth of detaile...
The interaction of coolant jets is significant in effusion settings as a result of the short streamw...
The interaction of coolant jets is significant in effusion settings as a result of the short streamw...
The desire to increase the efficiency, i.e., reduce the specific fuel consumption and raise the thru...
The continuous drive for ever higher turbine entry temperatures is leading to considerable interest ...
Modern research on gas turbine cooling continues to focus on the optimization of different cooling d...
Film cooling is a technique used to protect turbine blades or other surfaces from a high temperatur...
Film cooling is a technique used to protect turbine blades or other surfaces from a high temperatur...
The continuous drive for ever higher turbine entry temperatures is leading to considerable interest ...
Transpiration cooling represents the pinnacle of turbine cooling and is characterized by an intrinsi...
The present study aims to investigate the effectiveness of effusion film cooling on an adiabatic fla...
The continuing rise in turbine entry temperatures has necessitated the development of ever-more adva...
The continuing rise in turbine entry temperatures has necessitated the development of evermore advan...
The continuing rise in turbine entry temperatures has necessitated the development of evermore advan...
The continuing rise in turbine entry temperatures has necessitated the development of evermore advan...
This thesis presents CFD predictions of gas turbine film and effusion cooling. The dearth of detaile...
The interaction of coolant jets is significant in effusion settings as a result of the short streamw...
The interaction of coolant jets is significant in effusion settings as a result of the short streamw...
The desire to increase the efficiency, i.e., reduce the specific fuel consumption and raise the thru...
The continuous drive for ever higher turbine entry temperatures is leading to considerable interest ...
Modern research on gas turbine cooling continues to focus on the optimization of different cooling d...
Film cooling is a technique used to protect turbine blades or other surfaces from a high temperatur...
Film cooling is a technique used to protect turbine blades or other surfaces from a high temperatur...
The continuous drive for ever higher turbine entry temperatures is leading to considerable interest ...
Transpiration cooling represents the pinnacle of turbine cooling and is characterized by an intrinsi...
The present study aims to investigate the effectiveness of effusion film cooling on an adiabatic fla...