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Non-destructive Inspection of Composite Aileron during Fatigue Test

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F21%3AN0000025" target="_blank" >RIV/00010669:_____/21:N0000025 - isvavai.cz</a>

  • Result on the web

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

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.1051/matecconf/202134903016" target="_blank" >10.1051/matecconf/202134903016</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    Non-destructive Inspection of Composite Aileron during Fatigue Test

  • Original language description

    The operational safety and reliability of an airplane must be an integral part of its design. The use of suitable materials that pass material certification tests is very important for a new aircraft design. The next part is testing specific samples, sub-components, and components such as the aileron. The paper deals with a non-destructive evaluation of composite primary structural part fatigue tests in accordance with damage tolerance philosophy considering impact damage presence. NDT methods such as visual, eddy current, and ultrasonic testing included phased array technique, are used for the inspections. A schedule of inspections was created, and structural durability was verified.

  • 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/FW01010225" target="_blank" >FW01010225: Proof of L-39NG airframe with tripled fatigue life</a><br>

  • Continuities

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

Others

  • Publication year

    2021

  • Confidentiality

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

Data specific for result type

  • Article name in the collection

    6th International Conference of Engineering Against Failure (ICEAF-VI 2021)

  • ISBN

  • ISSN

    2261-236X

  • e-ISSN

    2261-236X

  • Number of pages

    6

  • Pages from-to

    nestrankovano

  • Publisher name

    MATEC Web of Conferences

  • Place of publication

  • Event location

    online

  • Event date

    Jun 23, 2021

  • Type of event by nationality

    EUR - Evropská akce

  • UT code for WoS article