Author:
LIU Xin,SHEN Xiuli,GONG Longdong,LI Peng
Subject
Mechanical Engineering,Aerospace Engineering
Reference23 articles.
1. Wen SQ, He AJ. Application of CMC on thermal parts of aeroengine. J Aeronaut Manuf Technol 2009; (Z): 4–7 [Chinese].
2. Vedula V, Shi J, Jarmon D, Zadrozny G. Ceramic matrix composite turbine vanes for gas turbine engines. ASME turbo expo: power for land, sea, and air; 2005 June 6–9; Reno, USA. New York: ASME; 2005. p. 247–51.
3. Brewer D, Verrilli M, Calomino A. Ceramic matrix composite vane subelement burst testing. ASME turbo expo: power for land, sea, and air; 2006 May 8–11; Barcelona, Spain. New York: ASME; 2006. p. 279–84.
4. Verrilli M, Calomino A, Robinson RC, Thomas DJ. Ceramic matrix composite vane subelement testing in a gas turbine environment. In: ASME turbo expo: power for land, sea, and air; 2004 June 14–17; Vienna, Austria. New York: ASME; 2004. p. 393–9.
5. Homogenization-based method for simulating micro-stress of 3D braided composites;Dong;J Acta Materiae Compositae Sinica,2005
Cited by
31 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献