E. Menga, C. López, S. Hernández, A. Baldomir, I. Romero, M. J. Sánchez

DOI Number: N/A

Conference number: IFASD-2017-132

This paper aims to review and explain fundamental tasks of the UQ process, particularly in the context of non-intrusive methods, which sample the deterministic model at points in the multidimensional input parameter space. Low Discrepancy Design (LDD) and Global Sensitivity Analysis (GSA) are shown to be effective analytical tools to define which parameters are relevant, the so-called Design Variables (DVs) and to quantify how the variance of the output is affected by the variance of the inputs. On the other side, especially for computationally expensive models, the direct use of the analytical model, i.e. Finite Element Model (FEM), can be extremely time-consuming. Hence, for complex systems, it is often necessary to generate first a meta-model and then, using it, complete the sensitivity analysis. The reliability and robustness of the method are demonstrated considering two structures with different level of complexity. In the first example the frequency response of a doble pinned beam is studied and discussed. In the second example the uncertain nonlinear vibrations of the RAM Air Inlet (RAI) system are considered. The stochastic reaction forces acting on the rods of the RAI mechanism are studied, considering prescribed density distributions on the interfaces, in terms of free-plays and stiffnesses, on the excitation force and on its dominant frequency. In this case the modal information is computed in NASTRAN and is translated to a MATLAB code, where the process is completed and the results evaluated. In both cases the relevant parameters are defined and the influence of each one on the variance of the output is clearly quantified. At the end of each example the results are discussed with a deep look at the physical coherence of the GSA Indices. Moreover, the second example gives the opportunity to discuss the use of Polynomial Chaos Expansion (PCE) meta-model in the frame of nonlinear vibration analysis.

Read the full paper here

Email
Print
LinkedIn
The paper above was part of  proceedings of a CEAS event and as such the author has signed a publication agreement to have their paper published in the repository. In the case this paper is found somewhere else CEAS always links to the other source.  CEAS takes great care in making the correct content available to the reader. If any mistakes are found  in the listings please contact us directly at papers@aerospacerepository.org and we will correct the listing promptly.  CEAS cannot be held liable either for mistakes in editorial or technical aspects, nor for omissions, nor for the correctness of the content. In particular, CEAS does not guarantee completeness or correctness of information contained in external websites which can be accessed via links from CEAS’s websites. Despite accurate research on the content of such linked external websites, CEAS cannot be held liable for their content. Only the content providers of such external sites are liable for their content. Should you notice any mistake in technical or editorial aspects of the CEAS site, please do not hesitate to inform us.