Combined loading of unreinforced and Z-pin reinforced composite pi joints: An experimental and numerical study
被引:4
作者:
Finlay, James G.
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Univ Michigan, Dept Aerosp Engn, Ann Arbor, MI 48109 USAUniv Michigan, Dept Aerosp Engn, Ann Arbor, MI 48109 USA
Finlay, James G.
[1
]
Waas, Anthony M.
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机构:
Univ Michigan, Dept Aerosp Engn, Ann Arbor, MI 48109 USA
Arizona State Univ, Sch Engn Matter Transport & Energy, Tempe, AZ USAUniv Michigan, Dept Aerosp Engn, Ann Arbor, MI 48109 USA
Waas, Anthony M.
[1
,3
]
Bartley-Cho, Jonathan
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Northrop Grumman Corp, Res & Dev, Aero Struct Design & Anal, Redondo Beach, CA 90278 USAUniv Michigan, Dept Aerosp Engn, Ann Arbor, MI 48109 USA
Bartley-Cho, Jonathan
[2
]
Muraliraj, Nav
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Northrop Grumman Corp, Res & Dev, Aero Struct Design & Anal, Redondo Beach, CA 90278 USAUniv Michigan, Dept Aerosp Engn, Ann Arbor, MI 48109 USA
Muraliraj, Nav
[2
]
机构:
[1] Univ Michigan, Dept Aerosp Engn, Ann Arbor, MI 48109 USA
[2] Northrop Grumman Corp, Res & Dev, Aero Struct Design & Anal, Redondo Beach, CA 90278 USA
[3] Arizona State Univ, Sch Engn Matter Transport & Energy, Tempe, AZ USA
Blind predictions of experimental responses of non-reinforced and z-pin reinforced composite pi joints were established using a progressive damage and failure model. The finite element model used a novel mixed-mode cohesive formulation to model intra-laminar and inter-laminar damage. A deliberate meshing strategy was used for cohesive interlayers to capture the interaction between intra- and inter-laminar damage modes. A smeared cohesive zone modeling approach was implemented to efficiently include the effects of z-pinning for the z-pin reinforced specimens. Using material properties obtained through experimental correlation of simpler joint configurations, blind predictions for large element specimens subjected to combined loading (axial compression and push-off loading) were established. To assess the predictive capabilities of the model, experimental and numerical comparisons were made in terms of load-displacement response, critical loads, and failure progression. Comparisons between the experimental results and predictions for the unreinforced joints were found to be in good agreement across the range of compressive loads tested. For the z-pin reinforced joints, initial responses were accurately predicted; however, ultimate loads and the toughening effect of the z-pin reinforcement was overpredicted.