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Simulation of Fatigue Crack Propagation in the Wing Main Spar Flange

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F18%3APU129818" target="_blank" >RIV/00216305:26210/18:PU129818 - isvavai.cz</a>

  • Result on the web

    <a href="http://dx.doi.org/10.13164/conf.read.2018.7" target="_blank" >http://dx.doi.org/10.13164/conf.read.2018.7</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.13164/conf.read.2018.7" target="_blank" >10.13164/conf.read.2018.7</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    Simulation of Fatigue Crack Propagation in the Wing Main Spar Flange

  • Original language description

    Simulation of fatigue crack growth in the bottom flange of twin turboprop commuter aircraft wing spar is described in this paper. Analysed crack propagation scenario represents real wing full-scale fatigue test failure. Computational model of bottom flange was prepared using three-dimensional fracture mechanics software FRANC3D. Calculation of crack growth under the variable amplitude loading was performed in AFGROW code using the NASGRO equation and Wheeler retardation model. It was verified with the results of wing spar specimen fatigue test and fractograpic analysis of fatigue fracture from this experiment. Computational model was applied in the prognostic algorithm of structure health monitoring system.

  • 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/TE02000032" target="_blank" >TE02000032: Advanced Aerostructures Research Centre</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

    13th Research and Education in Aircraft Design Conference

  • ISBN

    978-80-214-5696-9

  • ISSN

  • e-ISSN

  • Number of pages

    10

  • Pages from-to

    66-75

  • Publisher name

    Neuveden

  • Place of publication

    Neuveden

  • Event location

    Brno

  • Event date

    Nov 7, 2018

  • Type of event by nationality

    EUR - Evropská akce

  • UT code for WoS article