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Exact(9)
Pronounced strain rate effects on the axial stress strain response were observed for all specimen types.
Percent reduction in compressive strength and stiffness due to high temperature was similar for all specimen sizes.
Toughness was also different for the bag and tool sides of the panels for all specimen types.
The experimental data generated in the present study for all specimen geometries, as well as a complete biaxial failure envelope in σ1 σ2 stress space for this laminate configuration, are presented.
These experimental data were used in combination with finite element solutions for all specimen geometries to determine a 'critical distance', a quantity or parameter determined from the stress distribution surrounding the notch in combination with fatigue limit stress data from unnotched specimens.
For all specimen, the filaments seem distorted and sheared after cutting (Fig. 3a d).
Similar(51)
These operations were repeated for all the specimens herein considered.
Typical failure modes for all specimens were summarized and analyzed.
Good energy dissipation capacities were obtained for all specimens studied.
A formal loan form is required for all specimens going on loan, including in-house loans.
However, a significant increase in the degree of crystallinity was observed for all specimens versus that for virgin specimens.
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