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
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Czech description
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Classification
Type
D - Article in proceedings
CEP classification
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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
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ISSN
2261236X
e-ISSN
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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
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