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The adhesively-bonded joints were experimentally investigated under tensile loading.
Calculations were performed for two different laminates with various crack sizes under tensile loading.
Lifetimes under tensile loading of several hundreds hours at high temperatures are reported.
Under tensile loading, initial damage in a microstructure is localized in a single random trabecula.
The DTS is then applied to predict the mechanical properties of graphene papers under tensile loading.
The stiffness characteristics of these models under tensile loading condition were compared with the experimental results.
Experiments indicate that fracture under compressive loading exhibits distinct behaviors different from that under tensile loading.
Finite element analysis model was developed to simulate the material and arm structure under tensile loading.
In this article, single-L composite peel joints are investigated under tensile loading.
In this fd range, phase velocity increases under tensile loading and group velocity decreases.
Their load carrying capability and failure process under tensile loading were investigated experimentally.
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