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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2020, Vol. 41 ›› Issue (8): 223987-223987.doi: 10.7527/S1000-6893.2020.23987

• Solid Mechanics and Vehicle Conceptual Design • Previous Articles     Next Articles

Validation method for post-buckling analysis model of stiffened composite panels considering uncertainties

WANG Binwen, AI Sen, ZHANG Guofan, NIE Xiaohua, WU Cunli   

  1. Aircraft Strength Research Institute of China, Xi'an 710065, China
  • Received:2020-03-19 Revised:2020-03-26 Online:2020-08-15 Published:2020-05-11
  • Supported by:
    Civil Aircraft Scientific Research Project(MJ-2015-F-027)

Abstract: In the lightweight structural design of stiffened composite panels, uncertainties in the geometric and material parameters lead to the uncertainty of ultimate load carrying capacity. Therefore, it is necessary to consider these uncertainties in model validation. A method to validate the post-buckling finite element model of stiffened composite panels considering the uncertain factors is proposed. Based on the orthogonal experimental design, the significance analysis of the uncertainty parameters was first carried out to obtain significance parameters, followed by the acquisition of a surrogate model by the Kriging model to represent the post-buckling characteristics. The probability distribution of the post-buckling loads for the stiffened composite panel was achieved by Monte Carlo simulations, and the accuracy of the post-buckling model verified by experimental data. This validation approach can be applied to similar engineering cases.

Key words: composite materials, stiffened panels, post-buckling, uncertainties, model validation

CLC Number: