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Mathematical Problems in Engineering
Volume 2017, Article ID 2147830, 13 pages
https://doi.org/10.1155/2017/2147830
Research Article

Design of Thermal Barrier Coatings Thickness for Gas Turbine Blade Based on Finite Element Analysis

1State Key Laboratory for Strength and Vibration of Mechanical Structures, School of Aerospace Engineering, Xi’an Jiaotong University, Xi’an 710049, China
2Dongfang Steam Turbine Co., Ltd., Deyang 618000, China

Correspondence should be addressed to Xueling Fan; nc.ude.utjx.liam@gnileuxnaf

Received 8 May 2017; Accepted 5 June 2017; Published 6 July 2017

Academic Editor: Fabrizio Greco

Copyright © 2017 Biao Li et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

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