Open Access
MATEC Web Conf.
Volume 293, 2019
2019 7th Asia Conference on Mechanical and Materials Engineering (ACMME 2019)
Article Number 04006
Number of page(s) 4
Section Mechanical Engineering
Published online 25 September 2019
  1. Zhang Jiangang, Sun Renjun, Tang Changhong. The method of transferring aerodynamic load to FEM nodes for large airplane [J]. Mechanics in Engineering, 2017, 39(1):25–29 (In Chinese) [Google Scholar]
  2. MSC.Software Corporation. MSC.Nastran Aeroelastic Analysis User’s Guide [M]. MSC.Software Corporation, 2004. [Google Scholar]
  3. Zhang Jiangang. Study on the interpolation method to calculate the aircraft wing aerodynamic press distribution on FEM nodes [J]. Aeronautical Science & Technology, 2017, 28(12): 14–18. (In Chinese) [Google Scholar]
  4. Gao Shangjun, Yu Zhefeng, Wang Hai. Conversion of aerodynamic load based on spring-cantilever model with minimal strain energy criterion [J]. Aircraft Design, 2013, (6): 1–4(In Chinese) [Google Scholar]
  5. Lei Li, Han Qing, Zhong Xiaoping. Comparative Analysis of Conversion Distribution Methods for Wing Structural Node Loads [J]. Advances in Aeronautical Science and Engineering, 2014, 5(3):383–389 (In Chinese) [Google Scholar]
  6. Chen Quanli, Xiong Jianqi. Application of the load equivariant method on aircraft static strength test. Aircraft Engineering, 2005(1): 63–65 (In Chinese) [Google Scholar]
  7. Wang Zhuanli. FEM node load calculation of wing structure [J]. Hongdu Science and Technology, 2007(1): 7–14 (In Chinese) [Google Scholar]

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