2021
DOI: 10.1002/nme.6740
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Integral equations and model reduction for fast computation of nonlinear periodic response

Abstract: We propose a reformulation for a recent integral equations approach to steady‐state response computation for periodically forced nonlinear mechanical systems. This reformulation results in additional speed‐up and better convergence. We show that the solutions of the reformulated equations are in one‐to‐one correspondence with those of the original integral equations and derive conditions under which a collocation‐type approximation converges to the exact solution in the reformulated setting. Furthermore, we ob… Show more

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Cited by 3 publications
(8 citation statements)
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References 19 publications
(66 reference statements)
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“…( 105)). The FRC obtained via local computations of SSM at O (5) agrees with those obtained using global continuation methods involving the harmonic balance method (NLvib [46]) and collocation (coco [13]); the plot shows the displacement amplitude for in the x 3 direction at the tip of the beam (see Table 4 for computation times) relaxing these tolerances further has no effect on the continuation speed. Once again, the computation times in Table 4 indicate orders-of-magnitude higher speed in reliably approximating FRC via local SSMs computations in comparison with global techniques that involve collocation or spectral approximations.…”
Section: Von Kármán Beamsupporting
confidence: 58%
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“…( 105)). The FRC obtained via local computations of SSM at O (5) agrees with those obtained using global continuation methods involving the harmonic balance method (NLvib [46]) and collocation (coco [13]); the plot shows the displacement amplitude for in the x 3 direction at the tip of the beam (see Table 4 for computation times) relaxing these tolerances further has no effect on the continuation speed. Once again, the computation times in Table 4 indicate orders-of-magnitude higher speed in reliably approximating FRC via local SSMs computations in comparison with global techniques that involve collocation or spectral approximations.…”
Section: Von Kármán Beamsupporting
confidence: 58%
“…On a macrolevel, this wing example resembles a cantilevered beam and we expect a hardening type response. Indeed, the three FRCs at O(3), O (5), and O(7) converge toward a hardening-type response, as shown in Fig. 14b.…”
Section: Aircraft Wingmentioning
confidence: 75%
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