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Given these challenges, and in wake of the future model extensions, this work proposes a new computational approach that reduces computational demand, maintains result accuracy, provides modeling flexibility and enables future model enhancements.
At present, models predicting shell multistability are often characterised by a compromise between computational efficiency and result accuracy.
The theory implemented is compared with other micro-structural formulations: micro models and serial parallel mixing theory, in terms of result accuracy and computational cost.
Only a few are changed according to suggestions in order to balance result accuracy and computational cost.
Computational results have verified accuracy and effectiveness of the proposed method.
Computational results demonstrating the accuracy and efficiency that can be obtained with the use of these models is presented.
Computational results showing the accuracy and effectiveness of the method are given for a drop deformation and Rayleigh capillary instability.
The computational results demonstrate the accuracy for model problems and illustrate the feasibility for more complex aeroacoustic problems of the source extraction technique.
The computational results demonstrate high accuracy in terms of agreement with linear theory and excellent efficiency in the sense that cost is comparable to (and usually less than) explicit schemes.
For rotation, its range is usually very small and high accuracy computational results can be obtained using two interferometers' differential computation; for translation, the closed form solutions without rotational displacement's computational error's transmission are derived by making full use of all additional interferometers' information, so that the computational accuracy can be ensured.
Performance in terms of computational time and results accuracy of both methods are finally evaluated and compared in the case of a specific application: the simulation of Eddy Current Testing (ECT) inspection problems.
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