A method for performing efficient parametric dynamic analyses in large finite element models undergoing structural modifications

Abstract A typical task in an engineering office is to perform parametric analyses in which the response of the structure is studied when some changes are performed. These changes may be needed in the design phase, during manufacturing or even in service. Nowadays many structural analyses employ large and detailed finite element models on which the different scenarios are considered. Parametric analyses in these structures under dynamic loading mean many code executions, require significant computer resources, result in unmanageable files and block expensive licenses of professional programs. There is a need for efficient, simple procedures which allow to perform such analyses in short time, using few resources and, if possible, releasing professional program licenses. We present a new, simple method for accelerating the parametric analyses in large structures under dynamic loading. The procedure has some similarities to model reduction methods, but no condensation is employed; in fact it can be combined with such methods for even larger efficiency gains. The proposal uses the information of the whole system of equations but only processes those nodal degrees of freedom of interest to the analyst. All needed data are easily accessed in any commercial finite element program and the process takes place entirely outside it. Modifications are introduced in a real reduced modal space and the system is re-ortogonalized. The procedure is accurate and allows for nonproportional damping, addition or elimination of stiffness, of mass and of substructures. We show the performance of the method in two study cases. One consists of modifications in the wing model of an unmanned aerial vehicle. The other one consists in the study of solutions to improve the dynamic behavior of a large civil structure.

[1]  K. Bathe,et al.  The Mechanics of Solids and Structures - Hierarchical Modeling and the Finite Element Solution , 2011 .

[2]  Hamid Bahai,et al.  Eigenvalue inverse formulation for optimising vibratory behaviour of truss and continuous structures , 2002 .

[3]  Phill-Seung Lee,et al.  An accurate error estimator for Guyan reduction , 2014 .

[4]  Mark Richardson,et al.  FEA model updating using SDM , 2007 .

[5]  Qing-Hua Zeng,et al.  Highly Accurate Modal Method for Calculating Eigenvector Derivatives in Viscous Damping Systems , 1995 .

[6]  Ki-Ook Kim Hybrid dynamic condensation for eigenproblems , 1995 .

[7]  M. Naď,et al.  Structural dynamic modification of vibrating systems , 2007 .

[8]  Michiel E. Hochstenbach,et al.  A comparison of model reduction techniques from structural dynamics, numerical mathematics and systems and control , 2013 .

[9]  Joanne L. Walsh,et al.  A comparison of several methods for the calculation of vibration mode shape derivatives , 1986 .

[10]  Mario Lázaro,et al.  Computation of eigenvalues in proportionally damped viscoelastic structures based on the fixed-point iteration , 2012, Appl. Math. Comput..

[11]  E. Brigham,et al.  The fast Fourier transform and its applications , 1988 .

[12]  John E. Mottershead,et al.  Model Updating In Structural Dynamics: A Survey , 1993 .

[13]  E. Kreyszig,et al.  Advanced Engineering Mathematics. , 1974 .

[14]  R. Clough,et al.  Dynamics Of Structures , 1975 .

[15]  Manex Martinez-Agirre,et al.  Higher order eigensensitivities‐based numerical method for the harmonic analysis of viscoelastically damped structures , 2011 .

[16]  Praveena Nair Sivasankaran,et al.  Spatial network analysis to construct simplified wing structural models for Biomimetic Micro Air Vehicles , 2016 .

[17]  Ahmad Zhafran Ahmad Mazlan,et al.  Structural dynamic modification of an active suspended handle with a parallel coupled piezo stack actuator , 2016, J. Syst. Control. Eng..

[18]  J. L. Pérez-Aparicio,et al.  Multiparametric computation of eigenvalues for linear viscoelastic structures , 2013 .

[19]  Peter Avitabile,et al.  Twenty years of structural dynamic modification: A review , 2002 .

[20]  T. Caughey,et al.  Classical Normal Modes in Damped Linear Dynamic Systems , 1960 .

[21]  W. Hurty Dynamic Analysis of Structural Systems Using Component Modes , 1965 .

[22]  R. E. Spears,et al.  Approach for Selection of Rayleigh Damping Parameters Used for Time History Analysis , 2012 .

[23]  H. Nevzat Özgüven,et al.  Nonlinear Structural Modification and Nonlinear Coupling , 2014 .

[24]  Paul S. Wilke,et al.  Whole-spacecraft shock isolation system , 2002, SPIE Smart Structures and Materials + Nondestructive Evaluation and Health Monitoring.

[25]  L. Rayleigh,et al.  The theory of sound , 1894 .

[26]  Mark Richardson,et al.  COMPARISON OF ANALYTICAL AND EXPERIMENTAL RIB STIFFENER MODIFICATIONS TO A STRUCTURE , 1989 .

[27]  Daniel Rixen,et al.  Generalized mode acceleration methods and modal truncation augmentation , 2001 .

[28]  Zu-Qing Qu,et al.  Model Order Reduction Techniques with Applications in Finite Element Analysis , 2004 .

[29]  Paul Reynolds,et al.  Modal testing and FE model tuning of a lively footbridge structure , 2006 .

[30]  L. Majkut Eigenvalue based inverse model of beam for structural modification and diagnostics: theoretical formulation , 2010 .

[31]  Brian Schwarz,et al.  Structural Modifications Using Higher Order Elements , 1997 .

[32]  M. Bampton,et al.  Coupling of substructures for dynamic analyses. , 1968 .

[33]  K. Bathe Finite Element Procedures , 1995 .

[34]  Yuan-Cheng Fung,et al.  An introduction to the theory of aeroelasticity , 1955 .

[35]  Jimin He,et al.  Local structural modification using mass and stiffness changes , 1999 .

[36]  R. Guyan Reduction of stiffness and mass matrices , 1965 .