team:gdeliege:nnm
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team:gdeliege:nnm [2015/08/13 11:45] – geoffrey | team:gdeliege:nnm [2016/03/30 15:23] (current) – external edit 127.0.0.1 | ||
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This is one of the research topics of the | This is one of the research topics of the | ||
[[http:// | [[http:// | ||
- | Actually, I knew nothing | + | Actually, I knew nothing |
told me about it | told me about it | ||
and about the nonlinear equations he wanted to solve with finite elements. | and about the nonlinear equations he wanted to solve with finite elements. | ||
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$$ | $$ | ||
The domain boundary must be tangent to the velocity field to avoid problems with the definition of boundary conditions. Ludovic came up with clever and effective solutions to deal with this issue [1]. | The domain boundary must be tangent to the velocity field to avoid problems with the definition of boundary conditions. Ludovic came up with clever and effective solutions to deal with this issue [1]. | ||
- | Fig. 1 shows results I obtained with my code for a simple 2-DOF system, described in [1] | + | Fig. 1 shows results I obtained with my code for a simple 2-DOF system, |
{{ : | {{ : | ||
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[1] L. Renson, G. Deliége, G. Kerschen. //An effective finite-element-based method for the computation of nonlinear normal modes of nonconservative systems.// Meccanica, vol. 49(8), pp. 1901-1916, 2014. \\ | [1] L. Renson, G. Deliége, G. Kerschen. //An effective finite-element-based method for the computation of nonlinear normal modes of nonconservative systems.// Meccanica, vol. 49(8), pp. 1901-1916, 2014. \\ | ||
[2] L. Renson. //Nonlinear Modal Analysis of Conservative and Nonconservative Aerospace Structures.// | [2] L. Renson. //Nonlinear Modal Analysis of Conservative and Nonconservative Aerospace Structures.// | ||
+ | \\ | ||
+ | [[team: | ||
team/gdeliege/nnm.1439459114.txt.gz · Last modified: 2016/03/30 15:22 (external edit)