Novel Thermal Barrier Coating Materials
A special issue of Materials (ISSN 1996-1944). This special issue belongs to the section "Thin Films and Interfaces".
Deadline for manuscript submissions: closed (20 September 2023) | Viewed by 1399
Special Issue Editors
Interests: high temperature materials for aerospace applications; ceramic matrix composites materials; ceramic thermal protection system; re-entry & hypersonic systems and technologies; heat transfer; high speed aerodynamics; space technologies; manufacturing processes for aerospace industry
Special Issues, Collections and Topics in MDPI journals
Special Issue Information
Dear Colleagues,
Thermal barrier coatings (TBCs) are usually applied for protecting metallic components in gas turbines for aviation and energy applications. These hot components include combustion chambers, blades, and vanes. The TBC leads to a significant reduction of heat transfer from the high temperature gas to the metal surface. Research in new chemical compositions and the development of novel deposition processes, prediction of the TBC service life and of failure modes are key aspects for the TBC production process. In parallel, the improvement of experimental capabilities in the thermal, mechanical and relevant operative environment in conjunction with numerical modelling tools allow the enhancement in TBC understanding and their extensive usage for industrial applications.
In this Special Issue, research and development enhancement in the field of TBC from the chemical composition to deposition process including experimental and numerical aspects are presented and discussed.
It is my pleasure to invite you to submit a manuscript for this Special Issue. Full papers, communications, and reviews are all welcome.
Dr. Mario De Stefano Fumo
Dr. Mario Tului
Guest Editors
Manuscript Submission Information
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Keywords
- thermal barrier coating
- gas turbine
- new chemical composition
- deposition process
- experimental facilities
- numerical modelling
