Thermo-mechanical degradation and mitigation of molten volcanic ash wetting on thermal barrier coatings of jet engine turbine blades

Modern gas turbine engines employed in power and aerospace industries extensively utilize thermal barrier coatings (TBCs) to protect the structural integrity of engine components against any rapid degradation at extremely high temperatures (1300-1500 °C). TBCs typically consist of 7 wt% yttria-stabi...

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Bibliographic Details
Main Author: Lokachari, Siddharth
Format: Thesis
Language:English
Published: Ludwig-Maximilians-Universität München 2020
Subjects:
500
550
Online Access:https://dx.doi.org/10.5282/edoc.27010
https://edoc.ub.uni-muenchen.de/id/eprint/27038