Optimization design method for energy-absorbing composite structure with probabilistic uncertainty

被引:0
|
作者
Feng Z. [1 ]
Su X. [1 ]
Zhao Y. [1 ]
Xie J. [1 ]
Mou H. [1 ]
机构
[1] Key Lab of Civil Aircraft Airworthiness and Maintenance, CAAC, Tianjin
来源
关键词
Energy-absorbing characteristics; Optimization design; Programming algorithm; Thin-walled composite energy-absorbing structure; Uncertainty;
D O I
10.13465/j.cnki.jvs.2019.11.016
中图分类号
学科分类号
摘要
Due to larger dispersity of mechanical performance and lower machining precision of composite materials, thin-walled composite energy-absorbing structures have uncertainties hard to ignore. Here, an optimization design method for thin walled composite energy-absorbing structures with parametric uncertainty was established to identify parametric uncertainty in design stage and design thin walled composite structures with the optimal energy absorption feature. Firstly, parametric ranges were acquired according to using conditions, and the central combined test design was used to determine the test matrix of designed parameters, calculate the mean value and standard deviation of each group of designed parameters' energy absorption characteristic index in the test matrix, and determine response surface equations between different design parametric groups and mean values, standard deviations of their energy absorption indexes, respectively. Finally, the sequence quadratic programming algorithm was adopted to get an optimization solution after substituting response surface equations and design requirements into the optimized mathematical expression. A T700/3234 composite thin-walled circular tube was taken as a study object. Within the specified ranges of feature sizes, under the specified peak load, the maximum ratio energy-absorbing problem and the ratio energy-absorbing's minimum standard deviation problem were solved, respectively to verify the applicability of the proposed method. © 2019, Editorial Office of Journal of Vibration and Shock. All right reserved.
引用
收藏
页码:101 / 109and139
相关论文
共 11 条
  • [1] Fasanella E.L., Multi-terrain impact testing and simulation of a composite energy absorbing fuselage section, American Helicopter Society 60th Annual Forum, (2004)
  • [2] Mamalis A.G., Crashworthy characteristics of axially statically compressed thin-walled square CFRP composite tubes: experimental, Composite Structures, 63, pp. 347-360, (2004)
  • [3] Lu Z., Wang X., Feng X., Critiacl bucking load discrepancy of composite laminates, Acta Material Composite Sinica, 30, 1, pp. 194-200, (2013)
  • [4] Salehghaffari S., Raisrohani M., Evidence-based design optimization of energy absorbing components under material field uncertainty, 53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, (2012)
  • [5] Huang J., Wang X., Numerical and experimental investigations on the axial crushing response of composite tubes, Composite Structures, 91, pp. 222-228, (2009)
  • [6] Joosten M.W., Dutton S., Kelly D., Et al., Experimental and numerical investigation of the crushing response of an open section composite energy absorbing element, Composite Structures, 93, pp. 682-689, (2011)
  • [7] Mamalis A.G., Manolakos D.E., Viegelahn G.L., Crashworthy behaviour of thin-walled tubes of fibre glass composite materials subjected to axial loading, Journal of Composite Materials, 24, 1, pp. 72-91, (1990)
  • [8] Liang Z., Chen J., Zhu Z., Dynamic interval analysis for uncertain structures, Chinese Journal of Applied Mechanics, 25, 1, pp. 46-50, (2008)
  • [9] Jiang W., Jin H., Sun W., Aerodynamic optimization for winglets based on multilevel response surface method, Acta Aeronautica et Astrinautica Sinica, 31, 9, pp. 1746-1751, (2010)
  • [10] Xie J., Feng Z., Zhao Y., Et al., Evaluation method based on probability for energy-absorbing composite structures with uncertain parameters, Journal of Vibration and Shock, 34, 22, pp. 109-114, (2015)