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The method presented gives good results and can be used for modelling of turbomachine blades, aircraft propellers or helicopter rotor blades which may be considered as straight non-uniform beams with built-in pretwist.
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All methods presented give one overall treatment effect and are therefore not necessarily suitable in situations where the treatment effect for patients who switch onto a treatment is not the same as for those who were initially allocated to the experimental treatment arm.
A comparative analysis of the piezo-voltage dependence on the compressive strain, obtained from a previously reported description of the nanoribbon dynamics and from the more accurate molecular dynamics, reveals that the method here presented gives a more precise description of the effect of in-plane vibration of the atoms on the harvesting performance of the device.
Therefore in this study, a method of categorising disagreements was presented, given the intended usage of the application is IHC scoring.
Recently, we have developed a digital correction method, presented in [3], that gives good performances with a low complexity, even for large mismatches.
The new method presented in this paper gives theoretically unlimited spatial resolution by means of a very sparse array of stationary actuating/sensing elements.
The examples show that the accuracy improves by increasing the number of sinc grid points N. The method presented here is simple and gives a numerical solution, which is valid for various boundary conditions.
The synthesis method presented in this paper is given in the form of a linear matrix inequality-based optimization problem, which can be efficiently solved by a readily available software.
Following the method presented by Bonett [ 30], given 2 raters, a planning value of ICC = 0.87 and a desired 95% confidence interval (CI) with the width of 0.20, a minimum sample size of 29 participants was needed.
Compared with previous methods, the UDCA preparation methods presented herein (i) gave higher purity and recovery, (ii) avoided cumbersome procedures, (iii) was more cost efficient, and (iv) did not require harsh reaction conditions.
In this paper, a new method is presented that gives exact member-end-moments for continuous beams and bridge structures, without the need to distribute moments back and forth as in moment distribution or to set up and solve simultaneous equations, as with the stiffness method.
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Justyna Jupowicz-Kozak
CEO of Professional Science Editing for Scientists @ prosciediting.com