AbstractThe preconditioned density-based conjugate heat transfer (CHT) algorithm was used to investigate the heat transfer characteristics of a cooled turbine vane. Fluid domain provided boundary heat flux for solid domain and obtained boundary temperature from it for the coupling strategy. The governing equations were solved by the preconditioned density-based finite-volume method, with preconditioning matrix, improved Abu-Gharmam Shaw (AGS) transition model, matrix dissipation scheme and four kinds of turbulence models. The grid system is multi-block structured grids for fluid domain and unstructured grids for solid domain, with full-matched grids at the fluid–solid interfaces. The effects of turbulence model, outlet Mach number, outlet R...
A conjugate heat transfer solver has been developed and applied to a realistic film-cooled turbine v...
AbstractThe accurate simulation of boundary layer transition process plays a very important role in ...
In the present thesis the link between aerodynamics and heat transfer in high pressure turbines is i...
The preconditioned density-based conjugate heat transfer (CHT) algorithm was used to investigate the...
AbstractThe accurate simulation of boundary layer transition process plays a very important role in ...
Conjugate heat transfer analysis was performed to investigate the flow and cooling performance of th...
We report on work carried out to develop a 3-D coupled Finite Volume/BEM-based temperature forward/f...
International audienceGreat efforts are still put into the design process of advanced film-cooling c...
In this study, five models, including the standard k-epsilon (SKE), realizable k-epsilon (RKE), SST ...
There are different characters of air flow in a conventional gas turbine blade cooling channel. Thes...
The performance of modern heavy-duty gas turbines is greatly determined by the accurate numerical pr...
The performance of modern heavy-duty gas turbines is greatly determined by the accurate numerical pr...
The need to accurately predict heat transfer in aircraft anti-icing systems or in turbomachinery coo...
International audienceCHT (Conjugate Heat Transfer) is a main design constraint for GT (gas turbines...
International audienceCHT (Conjugate Heat Transfer) is a main design constraint for GT (gas turbines...
A conjugate heat transfer solver has been developed and applied to a realistic film-cooled turbine v...
AbstractThe accurate simulation of boundary layer transition process plays a very important role in ...
In the present thesis the link between aerodynamics and heat transfer in high pressure turbines is i...
The preconditioned density-based conjugate heat transfer (CHT) algorithm was used to investigate the...
AbstractThe accurate simulation of boundary layer transition process plays a very important role in ...
Conjugate heat transfer analysis was performed to investigate the flow and cooling performance of th...
We report on work carried out to develop a 3-D coupled Finite Volume/BEM-based temperature forward/f...
International audienceGreat efforts are still put into the design process of advanced film-cooling c...
In this study, five models, including the standard k-epsilon (SKE), realizable k-epsilon (RKE), SST ...
There are different characters of air flow in a conventional gas turbine blade cooling channel. Thes...
The performance of modern heavy-duty gas turbines is greatly determined by the accurate numerical pr...
The performance of modern heavy-duty gas turbines is greatly determined by the accurate numerical pr...
The need to accurately predict heat transfer in aircraft anti-icing systems or in turbomachinery coo...
International audienceCHT (Conjugate Heat Transfer) is a main design constraint for GT (gas turbines...
International audienceCHT (Conjugate Heat Transfer) is a main design constraint for GT (gas turbines...
A conjugate heat transfer solver has been developed and applied to a realistic film-cooled turbine v...
AbstractThe accurate simulation of boundary layer transition process plays a very important role in ...
In the present thesis the link between aerodynamics and heat transfer in high pressure turbines is i...