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Acta Armamentarii ›› 2014, Vol. 35 ›› Issue (10): 1619-1624.doi: 10.3969/j.issn.1000-1093.2014.10.015

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Experimental and Numerical Simulation on Deformation and Debonding Processes of HTPB Propellant/Liner Adhesive Specimen

JIANG Ai-min, LI Gao-chun, HUANG Wei-dong, QIU Xin   

  1. (Department of Aircraft Engineering, Naval Aeronautical and Astronautical University, Yantai 264001, Shandong, China)
  • Received:2013-10-28 Revised:2013-10-28 Online:2014-11-28
  • Contact: JIANG Ai-min E-mail:jiangaimin98@126.com

Abstract: In order to obtain the mechanical behavior and failure mode of interface, the uniaxial tension experiments are conducted on HTPB propellant/liner adhesive specimen. The deformation images of various stages are achieved, and the debonding process is observed macroscopically. A cohesive element model is adopted to simulate propellant/liner interface. The results show that the failure mode experiences damage initiation, damage evolution and debonding, and the stress-strain response of adhesive specimen has a distinct nonlinear characteristic. The simulated results of stress-strain response and deformation are consistent with the data obtained from experiment.

Key words: ordnance science and technology, adhesive specimen, debonding, cohesive element

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