• Title of article

    Nonlinear lap joint interface modeling and updating strategies for assembled structures

  • Author/Authors

    Shahabi ، Ehsan Center of Excellence in Experimental Solid Mechanics and Dynamics, School of Mechanical Engineering - Iran University of Science and Technology , Ahmadian ، Hamid Center of Excellence in Experimental Solid Mechanics and Dynamics, School of Mechanical Engineering - Iran University of Science and Technology

  • From page
    131
  • To page
    152
  • Abstract
    A comparison between two known strategies of modeling lap joint interfaces, namely, zerothickness and thin layer interface theories and their associated updating procedures, is made. Finite element models capable of accurately representing nonlinear behavior of assembled structures with localized nonlinearities in their bolted lap joint are developed. A practical strategy is employed in updating of these structures that initially parameters describing linear behavior are updated based on the lowamplitude excitation experimental observations. In the next step, parameters representing nonlinear effects are updated using steppedsine excitations near the structure resonance frequency. In both steps, the Particle Swarm Optimization (PSO) algorithm is used to reduce the discrepancies between experimental observations and model predictions. The identified contact interface models are validated by comparing their predictions with the experimental data not included in the updating procedure. In what concerns the updating process, the convergence rate of parameter identification in a model with zero thickness frictional contact elements was lower and more timeconsuming compared to the model with thin layer interfaces.This study shows assigning appropriate material properties for the thin interface layer results in contact forces with comparable accuracy to the ones obtained by zero thickness elements with less computational efforts.
  • Keywords
    Lap joint interface , Friction contact , Thin layer interface , Zero thickness element , Nonlinear frequency response
  • Journal title
    Journal of Theoretical and Applied Vibration and Acoustics
  • Journal title
    Journal of Theoretical and Applied Vibration and Acoustics
  • Record number

    2510541