In-situ X-ray tomography on permeability evolution of C/SiC porous ceramic for hypersonic vehicles
B Zhang, H Huang, S Wu, W Li, J Huang, A Lin… - Ceramics …, 2021 - Elsevier
Transpiration cooling system in hypersonic vehicles still remains a challenge due to the
limitations of observing permeability and microstructure evolution of porous medium filled …
limitations of observing permeability and microstructure evolution of porous medium filled …
Interfacial stresses of thermal barrier coating with film cooling holes induced by CMAS infiltration
To obtain high gas turbine efficiency, a film cooling hole is introduced to prevent the
destruction of thermal barrier coating systems (TBCs) due to hot gases. Furthermore …
destruction of thermal barrier coating systems (TBCs) due to hot gases. Furthermore …
Experimental and simulation analysis of the evolution of residual stress due to expansion via CMAS infiltration in thermal barrier coatings
The failure behavior of thermal barrier coatings (TBCs) involves multilayered systems
infiltrated with calcium–magnesium–alumino-silicates (CMAS). The metastable tetragonal …
infiltrated with calcium–magnesium–alumino-silicates (CMAS). The metastable tetragonal …
A three-dimensional finite element model for the oxide growth mechanism and growth-induced stress within thermal barrier system
L Cen, WY Qin, QM Yu - Materials Today Communications, 2021 - Elsevier
Thermal barrier coating is subjected to out-of-plane displacements and possible in-plane
cracks as thermally grown oxide (TGO) grows at high temperatures. Three different schemes …
cracks as thermally grown oxide (TGO) grows at high temperatures. Three different schemes …
Thermal stresses for a coated irregularly shaped hole embedded in an infinite substrate subject to a remote uniform heat flow
This article presents analytical solutions for a coated irregularly shaped void embedded in
an infinite substrate subject to remote uniform heat flow. Both the temperature and stress …
an infinite substrate subject to remote uniform heat flow. Both the temperature and stress …
[PDF][PDF] Interfacial Stresses of Thermal Barrier Coating with Film Cooling Holes Induced by CMAS Infiltration. Coatings 2022, 12, 326
To obtain high gas turbine efficiency, a film cooling hole is introduced to prevent the
destruction of thermal barrier coating systems (TBCs) due to hot gases. Furthermore …
destruction of thermal barrier coating systems (TBCs) due to hot gases. Furthermore …