@Article{cmc.2012.032.201,
AUTHOR = {A.J. de  Wit, D. Akçay Perdahcıoğlu, T.  Ludwig, W.M. van den Brink, A. de  Boer},
TITLE = {Generic Linking of Finite Element Models for Non-Linear Static and Global Dynamic Analyses of Aircraft Structures},
JOURNAL = {Computers, Materials \& Continua},
VOLUME = {32},
YEAR = {2012},
NUMBER = {3},
PAGES = {201--218},
URL = {http://www.techscience.com/cmc/v32n3/27912},
ISSN = {1546-2226},
ABSTRACT = {Depending on the type of analysis, Finite Element (FE) models of different fidelity are necessary. Creating these models manually is a labor intensive task. This paper discusses two approaches for generating FE models of different fidelity from a single reference FE model. The models are created with a single modelling and meshing toolkit. These different fidelity models are created for use with global-local non-linear static analysis and for use with dynamic linear sub-structuring reduction method. Efficiency of the developed approaches is demonstrated via non-linear static and modal analysis of a carbon-fiber stiffened panel.},
DOI = {10.3970/cmc.2012.032.201}
}