2016
DOI: 10.2514/1.j054036
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Modal Substructuring of Geometrically Nonlinear Finite-Element Models

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Cited by 42 publications
(18 citation statements)
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“…For example, NNMs have been used to understand the dynamic behaviour of full-scale aircraft and satellites [17,18], as a tool in substructuring [19] and the construction of reduced-order models [20], and for damage detection in engineering structures [21]. Along with such large-scale mechanical structures, NNMs have also seen successful application to MEMS devices [22], nanostructures [23] and to acoustic–structure interactions [24].…”
Section: Introductionmentioning
confidence: 99%
“…For example, NNMs have been used to understand the dynamic behaviour of full-scale aircraft and satellites [17,18], as a tool in substructuring [19] and the construction of reduced-order models [20], and for damage detection in engineering structures [21]. Along with such large-scale mechanical structures, NNMs have also seen successful application to MEMS devices [22], nanostructures [23] and to acoustic–structure interactions [24].…”
Section: Introductionmentioning
confidence: 99%
“…An example of linear problem in harmonic aeroacoustics with nonaffine dependence in the frequency is available in the work of Casenave et al Some nonlinearities can be treated without approximation, for example, the advection term is fluid dynamics (with a ROM based on a Galerkin method in our context) only requires the precomputation of an order‐3 tensor in the form normalΩψi·false(ψj·false)ψk, 1 ≤ i , j , k ≤ n , see the work of Akkari et al for the reduction of the nonlinear Navier‐Stokes equations, with an exact operator compression step. Other examples can be found in structural dynamics with geometric nonlinearities, where order‐2 and order‐3 tensors can be precomputed, see section 3.2 in the work of Kuether and the work of Mignolet et al…”
Section: Reduced Order Modelingmentioning
confidence: 99%
“…The parameter values used to obtain these plots for different values of k and ε were m 1 = m 2 = 1, with c = 0 and f 1 = 0. Here, the black solid lines describe the solutions obtained from Equations (34) and (35), while the colored, dashed lines represent the backbone curves computed from Equation (33). Equations (33) to (35).…”
Section: Of 22mentioning
confidence: 99%
“…Furthermore, nonlinear normal modes have been used to identify localized modes in micro-electromechanical devices [28] for the development of a new kind of low frequency acoustic absorber [29] and for the analysis of nonlinear vibrations for double-walled carbon nanotubes [30]. Also, the nonlinear normal modes have helped in the understanding of the dynamic response behavior of full-scale aircrafts and satellites [31,32] as a tool for sub-structuring [33], for the construction of reduced-order models [34], and for damage detection in engineering structures [35], among others uses.…”
Section: Introductionmentioning
confidence: 99%