2005
DOI: 10.1016/j.jsv.2004.08.036
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Nonlinear modal models for sonic fatigue response prediction: a comparison of methods

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Cited by 156 publications
(75 citation statements)
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“…Indeed, the displacement fields of these linear modes for shell-like structures are primarily transverse/normal to the structure and thus do not capture accurately the in-plane/tangential displacements that take place when the deformations are no longer infinitesimal. For example, if the structure is completely clamped, transverse deformations imply a stretching (referred to as the membrane stretching, see [1,3,6] for discussion) of the structure. For cantilevered structures, this effect is reflected by a shortening of the domain occupied by the structure in the undeformed configuration.…”
Section: Basis Selectionmentioning
confidence: 99%
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“…Indeed, the displacement fields of these linear modes for shell-like structures are primarily transverse/normal to the structure and thus do not capture accurately the in-plane/tangential displacements that take place when the deformations are no longer infinitesimal. For example, if the structure is completely clamped, transverse deformations imply a stretching (referred to as the membrane stretching, see [1,3,6] for discussion) of the structure. For cantilevered structures, this effect is reflected by a shortening of the domain occupied by the structure in the undeformed configuration.…”
Section: Basis Selectionmentioning
confidence: 99%
“…Notwithstanding the above difficulties, the ROM capabilities have progressed from applications to flat structures (see [2][3][4][5][6][7][8][9]), to moderately large motions of curved structures (see [10][11][12][13][14]). Further, the coupling of these nonlinear structural reduced order models with aerodynamics, either full or reduced order model has also been successfully demonstrated in [15][16][17].…”
Section: Introductionmentioning
confidence: 99%
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“…Reduced-order modeling has been shown to be a viable alternative for a range of loading and response conditions. [1][2][3][4][5][6][7][8] For a typical aerospace structure having 1 Senior Research Engineer, Structural Acoustics Branch, Associate Fellow AIAA. 2 Senior Structural Engineer, Senior Member AIAA.…”
Section: Introductionmentioning
confidence: 99%
“…Note that the nonlinear modal reduction used by the authors does not statically condense in-plane DoFs. 3 Therefore, a technique similar to the current approach, 10 but which identifies only transverse LNMs, would generate only part of the required basis.…”
mentioning
confidence: 99%