Thermal barrier coatings for aircraft gas turbines

Publisher Website

14 January 1980

proceedings article
Published by American Institute of Aeronautics and Astronautics (AIAA)

https://doi.org/10.2514/6.1980-302

Abstract

No abstract available

This publication has 1 reference indexed in Scilit:

Ceramic turbine components research and development. Part 2. evaluation of MCrAlY/ZrO/sub 2/ (Y/sub 2/O/sub 3/) thermal-barrier coatings exposed to simulated gas turbine environments. Final report
Published by Office of Scientific and Technical Information (OSTI) ,1980