Jet array impingement heat transfer in a rectangular cavity with effusion holes
Various researchers have studied jet array impingement heat transfer in
impingement/effusion cooling systems. However, there is a lack of research on …
impingement/effusion cooling systems. However, there is a lack of research on …
Optimizing thermal performance in internal passage cooling with extended rib: Applying response surface method with artificial neural networks
Efficient cooling technology is crucial for high-temperature gas turbines which are significant
applications in thermal processes particularly in industries such as power generation …
applications in thermal processes particularly in industries such as power generation …
Effect of mass flow ratios on the conjugate heat transfer of a metal turbine vane at medium temperature
To investigate the effect of mass flow ratios on the conjugate heat transfer of an air-cooled
turbine vane, the surface static pressure test experiments and heat transfer experiments at …
turbine vane, the surface static pressure test experiments and heat transfer experiments at …
Research for double wall cooling configuration with flower shaped ribs
Y Luan, L Zhang, L Yang, Y Yin, F Magagnato… - International Journal of …, 2023 - Elsevier
Excellent turbine cooling configuration protects turbine blade from the erosion of gas.
Double wall cooling is a new cooling method which contains film cooling and impingement …
Double wall cooling is a new cooling method which contains film cooling and impingement …
Effect of degradation of the thermal barrier coating on the cooling performance of vane in gas turbine
Film cooling and thermal barrier coatings are essential for the thermal protection of high
temperature gas turbines. Firstly, the degradation of the coating at the vane surface has …
temperature gas turbines. Firstly, the degradation of the coating at the vane surface has …
Experimental investigation on the combined cooling methods of jet impingement and film cooling for the pressure surface of the turbine vane leading cavity
To investigate the performance of impingement/film combined cooling methods on the
turbine vane pressure surface of leading cavity, typical cooling techniques and potential …
turbine vane pressure surface of leading cavity, typical cooling techniques and potential …
Study of Tangential Effusion Cooling of a Combustor Liner
Z Li, P Xie, Q Zeng, X Chen - Processes, 2023 - mdpi.com
Tangential effusion cooling of a combustor liner has a large difference from traditional
effusion cooling on a plate. In this paper, numerical simulation is carried out to study the flow …
effusion cooling on a plate. In this paper, numerical simulation is carried out to study the flow …
Thermal analysis of guide vanes with full double wall cooling structure with focusing on leading edge cooling
Z Xu, Z Xu, Y Chen - International Journal of Thermal Sciences, 2023 - Elsevier
In order to explore the thermal characteristics of the leading edge structure of the full double
wall cooling structure guide vane, a double wall cooling structure guide vane is established …
wall cooling structure guide vane, a double wall cooling structure guide vane is established …
The investigation of double wall cooling configuration with spherical cavity
L Zhang, Y Luan, L Yang, X Wu, T Sun… - … Communications in Heat …, 2024 - Elsevier
Double wall cooling is an efficient cooling method for turbine blade. Commonly used double
wall cooling configurations contains a cubic cavity between two walls. Chaos flow flied in the …
wall cooling configurations contains a cubic cavity between two walls. Chaos flow flied in the …
Comparisons of cooling performance and flow characteristics of a combustor liner plate with compound angle and simple angle effusion holes
The present investigation considers a unique compound angle arrangement, never
previously considered, with α= 30°, β=±30°, such that the compound angle of the effusion …
previously considered, with α= 30°, β=±30°, such that the compound angle of the effusion …