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Fatigue Disbonding Analysis of Wide Composite Panels by Means of Lamb Waves

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F18%3AN0000053" target="_blank" >RIV/00010669:_____/18:N0000053 - isvavai.cz</a>

  • Result on the web

    <a href="https://www.spiedigitallibrary.org/conference-proceedings-of-spie/10599/105991E/Fatigue-disbonding-analysis-of-wide-composite-panels-by-means-of/10.1117/12.2296851.short?SSO=1" target="_blank" >https://www.spiedigitallibrary.org/conference-proceedings-of-spie/10599/105991E/Fatigue-disbonding-analysis-of-wide-composite-panels-by-means-of/10.1117/12.2296851.short?SSO=1</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.1117/12.2296851" target="_blank" >10.1117/12.2296851</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    Fatigue Disbonding Analysis of Wide Composite Panels by Means of Lamb Waves

  • Original language description

    Guided wave-based monitoring of composite structures plays an important role in the area of structural health monitoring (SHM) of aerospace structures. Adhesively bonded joints have not yet fulfilled current airworthiness requirements; hence, assemblies of carbon fibre-reinforced parts still require mechanical fasteners, and a verified SHM method with reliable disbonding/delamination detection and propagation assessment is needed. This study investigated the disbonding/delamination propagation in adhesively bonded panels using Lamb waves during fatigue tests. Analyses focused on the proper frequency and mode selection, sensor placement and selection of parameter sensitive to the growth of disbonding areas. Piezoelectric transducers placed across the bonded area were used as actuators and sensors. Lamb wave propagation was investigated considering the actual shape of the crack front and the mode of the crack propagation. The actual cracked area was determined by ultrasonic A-scans. A correlation between the crack propagation rate and the A0 mode velocity was found.

  • Czech name

  • Czech description

Classification

  • Type

    D - Article in proceedings

  • CEP classification

  • OECD FORD branch

    20501 - Materials engineering

Result continuities

  • Project

  • Continuities

    I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Others

  • Publication year

    2018

  • Confidentiality

    S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Data specific for result type

  • Article name in the collection

    Proceedings of SPIE - The International SOciety for Optical Engineering, vol. 10599, art. no. 105991E

  • ISBN

    978-1-5106-1695-0

  • ISSN

    0277-786X

  • e-ISSN

    1996-756X

  • Number of pages

    7

  • Pages from-to

    nestrankovano

  • Publisher name

    SPIE

  • Place of publication

    Neuveden

  • Event location

    Denver, USA

  • Event date

    Mar 5, 2018

  • Type of event by nationality

    WRD - Celosvětová akce

  • UT code for WoS article

    000453067000033