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Full Scale Fatigue Test and Failure Analysis of Advanced Jet Trainer Wing

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F18%3AN0000120" target="_blank" >RIV/00010669:_____/18:N0000120 - isvavai.cz</a>

  • Result on the web

    <a href="https://www.matec-conferences.org/articles/matecconf/pdf/2018/47/matecconf_iceaf-v2018_04023.pdf" target="_blank" >https://www.matec-conferences.org/articles/matecconf/pdf/2018/47/matecconf_iceaf-v2018_04023.pdf</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.1051/matecconf/201818804023" target="_blank" >10.1051/matecconf/201818804023</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    Full Scale Fatigue Test and Failure Analysis of Advanced Jet Trainer Wing

  • Original language description

    A verification method for the fatigue life of the jet trainer wing with integrated fuel tanks is presented. The test was performed to identifythe critical points of the structure, to determine strain data and to proof fatigue life of the wing. During the test the non-destructive inspection methods for the identification and evaluation of the critical failures were employed; i.e. visual, ultrasonic and eddy current method. The failures were classified according to significance and reparability. The special test rig was designed to redistribute the load on the structure and to determine test data. The load control system MTS AeroST™ was used for fatigue test control. The fatigue load sequences with multilevel profiles of static and fatigue loading were applied. During the test, more than 230 failures were identified. The critical failures were repaired when found using two types of repair (metal and composite). The repairs were monitored during subsequent fatigue test run and evaluated to utilize in service.

  • 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/TH02010670" target="_blank" >TH02010670: Development of airframe for the L-39NG next generation aircraft</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. 04023

  • ISBN

  • ISSN

    2261-236X

  • e-ISSN

  • Number of pages

    9

  • Pages from-to

    nestrankovano

  • 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