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To ensure the launch tube design according with the theoretical design requirements, the stress and displacement of the launch tube under the maximum load were analyzed in comparison.
Static and cyclic creep, cyclic and linear construct stiffness, maximum load to failure, and displacement at maximum load were determined at time zero.
The crack opening and slip displacements at the maximum load were larger than those of the NP1F0 specimen having no steel fiber because the maximum load of the HP0F1 specimen was much higher than that of the NP1F0 specimen.
Overall numerical values of the maximum load were very close to experimental results, validating the numerical methodology to predict the lap shear strength and providing the necessary data to explain the obtained behaviour.
In these beams, the average values of deflection at maximum load were found to be equal to 6.3, 7.5 and 7.6 mm for control, one-ply and four-ply strengthened specimens, respectively (being 0.43, 0.41 and 0.08 mm the respective standard deviations).
The mode of failure, maximum displacement, number of cycles to failure, load at failure, and maximum load were recorded.
Similar(52)
The maximum load was 40 kilos.
The C-17's maximum load is 74.8 metric tons, according to Boeing.
The annual maximum load is 2850 MW.
The maximum load is 398 mN.
So the maximum load is the same.
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