Study on the effect of sample shapes on the thermal shock behavior of ZrB2-SiC-Graphite sharp leading edge

被引:8
作者
Wang A. [1 ,2 ]
Liao H. [1 ]
Zhang T. [1 ]
Jiang M. [1 ]
Guo F. [1 ]
Wang Y. [1 ]
机构
[1] School of Materials Science and Engineering, Nanjing Institute of Technology, Nanjing
[2] Jiangsu Key Laboratory of Advanced Structural Materials and Application Technology, Nanjing
关键词
fracture; sharp leading edges; thermal shock; ultra-high-temperature ceramic;
D O I
10.1002/ces2.10041
中图分类号
学科分类号
摘要
Reliable evaluation of the thermal shock behavior of sharp leading edges (SLEs) was hampered by a lack of available experimental method in past decades. Herein, a novel water spraying method was utilized to investigate the shape effect of ZrB2-SiC-Graphite SLEs during thermal shock. Experimental results indicated that the critical failure temperature of ZrB2-SiC-Graphite SLEs was most sensitive to the wedge angle, which could lead to a dramatic attenuation by about 35% from 12° to 9°, and was relatively little affected by the tip radius of curvature and the thickness. Simulation results further revealed that the decay of critical failure temperature was mainly due to the significant stress concentration caused by the reduction of wedge angle. Scanning electron microscopy observation proved that cracks tend to bypass graphite flakes due to their weak interfacial bonding, while branching always occurred when encountering hard phases or inclusions. © 2020 The Authors. International Journal of Ceramic Engineering & Science published by Wiley Periodicals, Inc. on behalf of American Ceramic Society.
引用
收藏
页码:101 / 109
页数:8
相关论文
共 47 条
[1]  
Zhu X.W., Zhao J.Q., Study on helium impingement cooling for a sharp leading edge subject to aerodynamic heating, Appl Therm Eng, 107, pp. 253-263, (2016)
[2]  
Padture N.P., Advanced structural ceramics in aerospace propulsion, Nat Mater, 15, (2016)
[3]  
Glass D., Physical challenges and limitations confronting the use of UHTCs on hypersonic vehicles, (2011)
[4]  
Cheng T.B., Li W.G., Thermal shock resistance of ultra-high-temperature ceramics under aerodynamic thermal environments, AIAAJ, 51, pp. 840-848, (2013)
[5]  
Farahbakhsh I., Ahmadi Z., Asl M.S., Densification, microstructure and mechanical properties of hot pressed ZrB<sub>2</sub>-SiC ceramic doped with nano-sized carbon black, Ceram Int, 43, pp. 8411-8417, (2017)
[6]  
Squire T.H., Marschall J., Material property requirements for analysis and design of UHTC components in hypersonic applications, J Eur Ceram Soc, 30, pp. 2239-2251, (2010)
[7]  
Zhang X., Liu R., Zhang X., Zhu Y., Sun W., Xiong X., Densification and ablation behavior of ZrB2 ceramic with SiC and/or Fe additives fabricated at 1600 and 1800 °C, Ceram Int, 42, 15, pp. 17074-17080, (2016)
[8]  
Jin H., Meng S., Zhang X., Zeng Q., Niu J., Effects of oxygen partial pressure on the oxidation of ZrB2–SiC–graphite composites at 1800 °C, Ceram Int, 42, 5, pp. 6480-6486, (2016)
[9]  
Fahrenholtz W.G., Hilmas G.E., Talmy I.G., Zaykoski J.A., Refractory diborides of zirconium and hafnium, J Am Ceram Soc, 90, pp. 1347-1364, (2007)
[10]  
Fahrenholtz W.G., Hilmas G.E., Oxidation of ultra-high temperature transition metal diboride ceramics, Int Mater Rev, 57, pp. 61-72, (2012)