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Because of the coupling between the bending and stretching equilibrium equations of FG plates, these plates have deflection under in-plane loads lower than the critical buckling load acting on the mid-plane.
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From load vs deflection curves, it is concluded that epoxy-repaired frames have maximum deflection under control in comparison to bare RC frames.
From load versus deflection curves, it is concluded that epoxy repaired frames have maximum deflection under control in comparison to bare RC frames.
In particular, the effect that key parameters have on deflection ratios and horizontal strains are investigated.
Also, the finite element analysis shows that the models with greater SAMI thickness have greater deflection.
For the same load, epoxy repaired frames have comparable deflection than similar braced frames.
The directional sampling problem is further emphasized by the low energy ion data, below 50 eV, which does not have entrance deflection scanning and is thus two-dimensional.
The trajectory of a launch vehicle is controlled by the thrust which can only have limited deflection angles with the vehicle longitudinal axis.
Because variation in brain shape was observed and may have biased deflection measurements, a second method of characterization was also used: a dorsal-ventral linear displacement ratio between CoMOL and the CoMbrain.
SRBBs have larger deflections but higher ultimate loads compared with SRSBs in static bending tests.
All three elements have large deflections and stress stiffening capabilities which are required for an eigenvalue and non-linear buckling analysis.
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