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Dynamic tests of composite panels of an aircraft wing

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F15%3APU114310" target="_blank" >RIV/00216305:26210/15:PU114310 - isvavai.cz</a>

  • Result on the web

    <a href="http://www.sciencedirect.com/science/article/pii/S0376042115000366" target="_blank" >http://www.sciencedirect.com/science/article/pii/S0376042115000366</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.1016/j.paerosci.2015.05.005" target="_blank" >10.1016/j.paerosci.2015.05.005</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    Dynamic tests of composite panels of an aircraft wing

  • Original language description

    The paper describes the analysis of aerospace composite structures under dynamic loading. Today, it is common to use design procedures based on assumption of static loading only, and dynamic loading is rarely assumed and applied in design and certification of aerospace structures. The paper describes the application of dynamic loading for the design of aircraft structures, and the validation of the procedure on a selected structure. The goal is to verify the possibility of reducing the weight through improved design/modelling processes using dynamic loading instead of static loading. The research activity focuses on the modelling and testing of a composite panel representing a local segment of an aircraft wing section, investigating in particular the buckling behavior under dynamic loading. Finite Elements simulation tools are discussed, as well as the advantages of using a digital optical measurement system for the evaluation of the tests. The comparison of the finite element simulations with the results of the tests is presented.

  • Czech name

  • Czech description

Classification

  • Type

    J<sub>x</sub> - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)

  • CEP classification

    JU - Aeronautics, aerodynamics, aeroplanes

  • OECD FORD branch

Result continuities

  • Project

  • Continuities

    R - Projekt Ramcoveho programu EK

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

    PROGRESS IN AEROSPACE SCIENCES

  • ISSN

    0376-0421

  • e-ISSN

  • Volume of the periodical

    2015

  • Issue of the periodical within the volume

    78

  • Country of publishing house

    US - UNITED STATES

  • Number of pages

    12

  • Pages from-to

    50-61

  • UT code for WoS article

    000364259300006

  • EID of the result in the Scopus database