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Effect of interlaminar flaw on composite panel behaviour under acoustic loading

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F18%3AN0000091" target="_blank" >RIV/00010669:_____/18:N0000091 - isvavai.cz</a>

  • Result on the web

    <a href="https://www.matec-conferences.org/articles/matecconf/abs/2018/47/matecconf_iceaf-v2018_01005/matecconf_iceaf-v2018_01005.html" target="_blank" >https://www.matec-conferences.org/articles/matecconf/abs/2018/47/matecconf_iceaf-v2018_01005/matecconf_iceaf-v2018_01005.html</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.1051/matecconf/201818801005" target="_blank" >10.1051/matecconf/201818801005</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    Effect of interlaminar flaw on composite panel behaviour under acoustic loading

  • Original language description

    A design of airframe structures has to be accompanied by material properties testing. Special focus has to be laid on high frequency fatigue behaviour. The acoustic fatigue test equipment for grazing wave’s incidence was designed based on the FE analyses. Flat composite panels were designed and manufactured using the Hexply 8552/AGP193-PW prepreg with different fiber lay-ups and with simulation of production imperfections or operational damage. Dynamic behaviour of panels was tested using three regimes of acoustic loading: white noise spectrum, engine noise spectrum and discrete harmonic frequencies loading. Rayleigh damping coefficients were evaluated for later use in FE models. Panel health was checked periodically through a power spectral density response on white noise signal. The ultrasonic NDT instruments were used for monitoring of relevant delamination increment. No increments of delamination were detected. The available acoustic power was below the fatigue limit of the tested structure.

  • Czech name

  • Czech description

Classification

  • Type

    D - Article in proceedings

  • CEP classification

  • OECD FORD branch

    20304 - Aerospace engineering

Result continuities

  • Project

    <a href="/en/project/TE02000032" target="_blank" >TE02000032: Advanced Aerostructures Research Centre</a><br>

  • Continuities

    P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

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

    MATEC Web of Conferences, vol. 188, art. no. 01005

  • ISBN

  • ISSN

    2261236X

  • e-ISSN

  • Number of pages

    8

  • Pages from-to

    nestránkováno

  • Publisher name

    EDP Sciences

  • Place of publication

    Neuveden

  • Event location

    ostrov Chios, Řecko

  • Event date

    Jun 20, 2018

  • Type of event by nationality

    EUR - Evropská akce

  • UT code for WoS article