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Experimental and Numerical Analyses of Optimized Composite Profiles for Aircraft Construction

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21110%2F22%3A00350407" target="_blank" >RIV/68407700:21110/22:00350407 - isvavai.cz</a>

  • Alternative codes found

    RIV/68407700:21220/22:00350407

  • Result on the web

    <a href="https://doi.org/10.1007/s11029-022-10029-y" target="_blank" >https://doi.org/10.1007/s11029-022-10029-y</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.1007/s11029-022-10029-y" target="_blank" >10.1007/s11029-022-10029-y</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    Experimental and Numerical Analyses of Optimized Composite Profiles for Aircraft Construction

  • Original language description

    The paper provides a description of the design, finite element analysis and testing of two optimized composite profiles intended primarily for the joining of aircraft structures. Profiles with T and Y shapes were manufactured using thermoforming technology via the one-shot process from a C/PPS (carbon fiber, polyphenylene sulfide matrix) fabric. Such profiles are usually loaded in the pull of direction. Finite element analysis was performed aimed at proving that the profiles were able to withstand the prescribed ultimate load without incurring damage. Static and fatigue testing was conducted on both profiles for the determination of strength and the construction limits with the similar result as from FE simulation - both profiles can withstand prescribed load without damage.

  • 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

    20302 - Applied mechanics

Result continuities

  • Project

    <a href="/en/project/FV30033" target="_blank" >FV30033: Design and manufacturing process development of primary aircraft parts of advanced shapes of reinforced thermoplastics</a><br>

  • Continuities

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

Others

  • Publication year

    2022

  • Confidentiality

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

Data specific for result type

  • Name of the periodical

    Mechanics of Composite materials

  • ISSN

    0191-5665

  • e-ISSN

    1573-8922

  • Volume of the periodical

    58

  • Issue of the periodical within the volume

    2

  • Country of publishing house

    DE - GERMANY

  • Number of pages

    10

  • Pages from-to

    283-292

  • UT code for WoS article

    000797778300002

  • EID of the result in the Scopus database

    2-s2.0-85130220238