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Figure 19 Lines and spaces processed by DLC-coated tips (load: 1,600 nN; line period: 80 nm).
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Cartesian large deflection solutions are given for general tip point loading, as well as a new closed form solution for the case of a large end-force only.
The problem of determining the parametric large deflection components of Euler Bernoulli cantilever beams subjected to combined tip point loading is studied in this paper.
Exploiting these solutions as theoretical tools we study the beam's angular and axial deflections behavior for several tip point loading conditions.
For static analysis, we have testified the model under a constant tip load.
The frame is subjected to a tip load which lies in an uncertainty domain with regard to its magnitude and direction.
The influence of the applied load ratio on the true crack-tip load ratio has been investigated for three different applied load ratios.
In this paper a comprehensive study is presented on the influence of rotatory inertia, shear deformation and tip load on the vibration behavior of one-link flexible manipulators.
A new analytical model for a functionally graded material FGM)/shape memory alloy (SMA) laminated composite cantilever beam subjected to a concentrated tip load is developed.
It has also been found that, in certain cases, the tip load has a profound effect on the vibration behavior of flexible manipulators.
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