Simulation of particle erosion to thermal barrier coatings with columnar and lamellar microstructure
Thermal barrier coating (TBC) is widely used in the hot sections of aircraft engines or gas turbines to extend componentslife.The surface layer of TBC is typically made of yttria-stabilized zirconia (YSZ),which is made by electron beam physical vapor deposition (EB-PVD) or Air Plasma Spray (APS).These two kinds of TBC have very different anti-erosion ability because of their different microstructure.
solid particle impact TBC surface densification residual stress erosion resistance
Yuan Yan Tiejun Wang Xi Chen Weixu Zhang
International Center for Applied Mechanics,State Key Laboratory for the Strength and Vibration of Me School of Aerospace,Xian Jiaotong University,Xian 710049,China International Center for Applied Mechanics,State Key Laboratory for the Strength and Vibration of Me
国际会议
北京
英文
1-1
2013-06-16(万方平台首次上网日期,不代表论文的发表时间)