Creator:
Yan, Jinrong
Date:
2022
Abstract:
The premature failure of the thermal barrier coatings (TBCs) system is a preliminary phenomenon that can significantly limit their applications in gas turbine engines. The delamination of TBCs occurs typically at interfaces between the top coat and bond coat due to thermal mismatch stress via both crack nucleation and propagation and decohesion. In this thesis, this phenomenon was studied using a multi-physics approach...exceeding text limit
Subject:
Engineering - Aerospace
Language:
English
Publisher:
Carleton University
Identifier:
Thesis Degree Name:
Master of Applied Science:
M.App.Sc.
Thesis Degree Level:
Master's
Thesis Degree Discipline:
Engineering, Aerospace
Parent Collection:
Theses and Dissertations