Open Access
MATEC Web Conf.
Volume 108, 2017
2017 International Conference on Mechanical, Aeronautical and Automotive Engineering (ICMAA 2017)
Article Number 02004
Number of page(s) 5
Section Material Analysis and Processing
Published online 31 May 2017
  1. Cui, H.-t., H.-q. Ma, and W.-d. Wen, Reliability-Based Shape Optimization of Tenon/Mortise in Aero-engines with Contact. Chinese Journal of Aeronautics, 2003. 16(4): p. 193–197. [CrossRef] [Google Scholar]
  2. Wang, P., et al., Effects of One-side-deviation on the Stress Distribution for the Aero-Engine Turbine Joint Structure. Gas Turbine Technology, 2014. [Google Scholar]
  3. Wang, S.F., et al., Effects of contact gap on contact properties of turbine blade tenon /mortise. Tuijin Jishu/journal of Propulsion Technology, 2015. 36(1): p. 112–118. [Google Scholar]
  4. Liao, H., et al. Multidisciplinary Optimization Technology Research on Typical Turbine Assembly Structure. in ASME 2014 International Mechanical Engineering Congress and Exposition. 2014. [Google Scholar]
  5. Shen, X.L., et al., SHAPE OPTIMIZATION OF AERO ENGINE FIR-TREE TENON/MORTISE STRUCTURE. Engineering Mechanics, 2011. 28(12): p. 231–237. [Google Scholar]
  6. Yang, M.C. and S.Y. Sun, Structural optimization of turbine tenon/mortise. Journal of Aerospace Power, 2010. 25(8): p. 1876–1882. [Google Scholar]

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