Filters
  • Collections
  • Group objects
  • File type

Search for: [Abstract = "Thermal barrier coatings \(TBCs\) are widely used on different hot components of gas turbine engines such as blades and vanes. Although, several mechanisms for the failure of the TBCs have been suggested, it is largely accepted that the durability of these coatings is primarily determined by the residual stresses that are developed during the thermal cycling."]

Number of results: 1

items per page

This page uses 'cookies'. More information