Abstract
Several recent studies (Mayes, R.L., Pacini, B.R., Roettgen, D.R.: A modal model to simulate typical structural dynamics nonlinearity. In: Proceedings of the 34th International Modal Analysis Conference. Orlando, FL, (2016); Pacini, B.R., Mayes, R.L., Owens, B.C., Schultz, R.: Nonlinear finite element model updating, part I: experimental techniques and nonlinear modal model parameter extraction. In: Proceedings of the 35th international modal analysis conference, Garden Grove, CA, (2017)) have investigated predicting nonlinear structural vibration responses using modified modal models. In such models, a nonlinear element is added in parallel to the traditional linear spring and damping elements. This assumes that the mode shapes do not change with amplitude and there are no interactions between modal degrees of freedom. Previous studies have predominantly applied this method to idealistic structures. In this work, the nonlinear modal modeling technique is applied to a more realistic industrial aerospace structure which exhibits complex bilinear behavior. Linear natural frequencies, damping values, and mode shapes are first extracted from low level shaker testing. Subsequently, the structure is excited using high level tailored shaker inputs. The resulting response data are modally filtered and used to empirically derive the nonlinear elements which, together with their linear counterparts, comprise the nonlinear modal model. This model is then used in both modal and physical domain simulations. Comparisons to measured data are made and the performance of the nonlinear modal model to predict this complex bilinear behavior is discussed.
Sandia National Laboratories is a multimission laboratory managed and operated by National Technology and Engineering Solutions of Sandia, LLC., a wholly owned subsidiary of Honeywell International, Inc., for the U.S. Department of Energy,s National Nuclear Security Administration under contract DE-NA-0003525.
Notice: This manuscript has been authored by National Technology and Engineering Solutions of Sandia, LLC. under Contract No. DE-NA0003525 with the U.S. Department of Energy/National Nuclear Security Administration. The United States Government retains and the publisher, by accepting the article for publication, acknowledges that the United States Government retains a non-exclusive, paid-up, irrevocable, world-wide license to publish or reproduce the published form of this manuscript, or allow others to do so, for United States Government purposes.
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Abbreviations
- c :
-
Damping coefficient
- c :
-
Vector of nonlinear coefficients
- f :
-
Frequency in cycles/sec
- f d,nl :
-
Nonlinear damping force
- f q :
-
Modal excitation force
- f qrfs :
-
Vector of nonlinear restoring forces, time domain
- F qrfs :
-
Vector of nonlinear restoring forces, frequency domain
- f rfs,nl :
-
Nonlinear restoring force
- f s,nl :
-
Nonlinear stiffness force
- H :
-
Frequency response function matrix
- j:
-
Imaginary number variable
- k :
-
Stiffness coefficient
- p :
-
Matrix of modal responses, time domain
- P :
-
Matrix of modal responses, frequency domain
- q :
-
Modal degree of freedom
- t :
-
Time
- x :
-
Physical displacement degree of freedom
- ζ:
-
Modal damping ratio
- ω :
-
Frequency in radians per second
- φ dp :
-
Drive point mode shape value
- \( \overline{\boldsymbol{\Psi}} \) :
-
Modal filter vector
- +:
-
Moore-Penrose pseudo-inverse of a matrix
References
Mayes, R.L., Pacini, B.R., Roettgen, D.R.: A modal model to simulate typical structural dynamics nonlinearity. In: Proceedings of the 34th International Modal Analysis Conference. Orlando, FL (2016)
Pacini, B.R., Mayes, R.L., Owens, B.C., Schultz, R.: Nonlinear finite element model updating, part I: experimental techniques and nonlinear modal model parameter extraction. In: Proceedings of the 35th international modal analysis conference, Garden Grove, CA (2017)
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Mayes, R.L., Johansen, D.D.: A modal parameter extraction algorithm using best-fit reciprocal vectors. In: Proceedings of the 16t International modal analysis conference, Santa Barbara, CA (1998)
Feldman, M.: Hilbert transform applications in mechanical vibration, pp. 241–244. Wiley, Chichester (2011)
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© 2019 The Society for Experimental Mechanics, Inc.
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Pacini, B.R., Holzmann, W.A., Mayes, R.L. (2019). Performance of Nonlinear Modal Model in Predicting Complex Bilinear Stiffness. In: Kerschen, G. (eds) Nonlinear Dynamics, Volume 1. Conference Proceedings of the Society for Experimental Mechanics Series. Springer, Cham. https://doi.org/10.1007/978-3-319-74280-9_8
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DOI: https://doi.org/10.1007/978-3-319-74280-9_8
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