Journal of Projectiles, Rockets, Missiles and Guidance >
Parameters Investigation of Lap Structure Between Skirt andComposite Material Case of SRM
Received date: 2014-07-29
Online published: 2025-05-30
Five parameters of lap structure between skirt and composites material cases of SRM were investigated using Artificial Neural Network algorithm.The objective function employed in the present work was the max strain along the fiber in the fibrous composites layers which outside the skirt under the case of SRM bearing the 400 t thrust loading.Simulation-based of design of experiment (DOE) was applied to simulate the five parameters.A sample of 27 cases, different from the previous ones, was used to validate the ANN.Finally, the objective function vs.design variables curves were plotted, and the parameters sensitivity analysis were carried out.
CHEN Ke , REN Quanbin , YOU Junfeng , WANG Liqiang . Parameters Investigation of Lap Structure Between Skirt andComposite Material Case of SRM[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2016 , 36(1) : 103 -106 . DOI: 10.15892/j.cnki.djzdxb.2016.01.026
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