• DocumentCode
    2911791
  • Title

    High-fidelity modeling for health monitoring in honeycomb sandwich structures

  • Author

    Luchinsky, Dmitry G. ; Hafiychuk, Vasyl ; Smelyanskiy, Vadim ; Tyson, RichardW ; Walker, James L. ; Miller, Jimmy L.

  • Author_Institution
    Mission Critical Technol. Inc., Segundo, CA, USA
  • fYear
    2011
  • fDate
    5-12 March 2011
  • Firstpage
    1
  • Lastpage
    7
  • Abstract
    High-Fidelity Model of the sandwich composite structure with real geometry is reported. The model includes two composite facesheets, honeycomb core, piezoelectric actuator/sensors, adhesive layers, and the impactor. The novel feature of the model is that it includes modeling of the impact and wave propagation in the structure before and after the impact. Results of modeling of the wave propagation, impact, and damage detection in sandwich honeycomb plates using piezoelectric actuator/sensor scheme are reported. The results of the simulations are compared with the experimental results. It is shown that the model is suitable for analysis of the physics of failure due to the impact and for testing structural health monitoring schemes based on guided wave propagation.
  • Keywords
    adhesives; condition monitoring; electric sensing devices; honeycomb structures; impact (mechanical); maintenance engineering; piezoelectric actuators; plates (structures); structural engineering; adhesive layers; damage detection; guided wave propagation; health monitoring; high-fidelity modeling; honeycomb core; honeycomb sandwich structures; impact propagation; impactor; piezoelectric actuator; piezoelectric sensors; sandwich honeycomb plates; structural health monitoring; wave propagation; Actuators; Analytical models; Materials; Monitoring; Numerical models; Propagation; Sensors;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2011 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    978-1-4244-7350-2
  • Type

    conf

  • DOI
    10.1109/AERO.2011.5747569
  • Filename
    5747569