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Predicted stiffness loss due to delamination in filament wound composite cylinders

Technical Report ·
OSTI ID:5360289
;  [1];  [2]
  1. Texas A and M Univ., College Station, TX (United States). Dept. of Aerospace Engineering
  2. Lawrence Livermore National Lab., CA (United States)
Three dimensional finite element analysis is used in conducting several case studies on the effect of delamination on the structural properties of various two-ply composite cylinders loaded in axial tension. In all cases, the effect of the damage is quantified through a reduction in axial stiffness of the cylinder. Two different crack geometries (circumferential and axial) and several different layups are considered. The results presented include stiffness, compliance, and energy release rate (ERR) as functions of crack length. 10 refs., 15 figs.
Research Organization:
Lawrence Livermore National Lab., CA (United States)
Sponsoring Organization:
DOE; USDOE, Washington, DC (United States)
DOE Contract Number:
W-7405-ENG-48
OSTI ID:
5360289
Report Number(s):
UCRL-CR-106325; ON: DE91017440
Country of Publication:
United States
Language:
English