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Compression after impact and fatigue behaviour of CFRP stiffened panels

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F15%3A%230001898" target="_blank" >RIV/00010669:_____/15:#0001898 - isvavai.cz</a>

  • Result on the web

    <a href="http://www.emeraldinsight.com/doi/full/10.1108/IJSI-06-2014-0030" target="_blank" >http://www.emeraldinsight.com/doi/full/10.1108/IJSI-06-2014-0030</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.1108/IJSI-06-2014-0030" target="_blank" >10.1108/IJSI-06-2014-0030</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    Compression after impact and fatigue behaviour of CFRP stiffened panels

  • Original language description

    Impact and fatigue are critical loading conditions for composite aerostructures. Compression behavior after impact and fatigue is a weak point for composite fuselage panels. The purpose of this paper is to characterize experimentally the compression behavior of carbon fiber reinforced plastic (CFRP) stiffened fuselage panels after impact and fatigue. The panels were tested using ultrasound inspection just after manufacturing to check material quality and between different tests to detect impact and fatigue damage accumulation. During tests the mechanical behavior of the panel was monitored using an optical displacement measurement system. Experimental results show that the presence of impact damage significantly degrades the compression behavior of thepanels. Moreover, the combined effect of BVID and fatigue was proven more severe than VID. The paper gives information about the compression after impact and fatigue behavior of CFRP fuselage stiffened panels, which represent the most re

  • Czech name

  • Czech description

Classification

  • Type

    J<sub>imp</sub> - Article in a specialist periodical, which is included in the Web of Science database

  • CEP classification

  • OECD FORD branch

    20304 - Aerospace engineering

Result continuities

  • Project

  • Continuities

    I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Others

  • Publication year

    2015

  • Confidentiality

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

Data specific for result type

  • Name of the periodical

    International Journal of Structural Integrity

  • ISSN

    1757-9864

  • e-ISSN

    1757-9872

  • Volume of the periodical

    6

  • Issue of the periodical within the volume

    2

  • Country of publishing house

    GB - UNITED KINGDOM

  • Number of pages

    18

  • Pages from-to

    176-193

  • UT code for WoS article

    000214188800003

  • EID of the result in the Scopus database

    2-s2.0-84928480400