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VERIFICATION AND NUMERICAL SIMULATION OF ADVANCED COMPOSITE INLET IN COMPLIANCE OF AIRWORTHINESS IMPACT REQUIREMENTS

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F19%3A00330362" target="_blank" >RIV/68407700:21220/19:00330362 - isvavai.cz</a>

  • Result on the web

    <a href="http://dx.doi.org/10.13164/conf.read.2018.1" target="_blank" >http://dx.doi.org/10.13164/conf.read.2018.1</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.13164/conf.read.2018.1" target="_blank" >10.13164/conf.read.2018.1</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    VERIFICATION AND NUMERICAL SIMULATION OF ADVANCED COMPOSITE INLET IN COMPLIANCE OF AIRWORTHINESS IMPACT REQUIREMENTS

  • Original language description

    Bird or hail stone strikes are an important phenomenon which must be considered during aircraft design. Most of major bird or hail strike incidents result from engine ingestion. As engines are the sole thrust providing mechanisms of an aircraft, it is critical to investigate and mitigate the effects of bird or hail strikes on engine inlets and systems to the greatest extent possible. The article presents application of test verified numerical simulation for design and full-scale test verification of advanced composite air inlet for new generation of jet trainer aircraft from point of view of high speed impact resistance. The physical bird and hail impact tests were performed at the Czech Aerospace Research Centre (VZLU) according to airworthiness requirements. The measurement during impact test were performed by high-speed camera, Fiber Bragg Grating (FGB) sensors and strain gauges in cooperation with Czech Technical University (CTU) in Prague. The results from full-scale bird and hail strike tests were compared with numerical simulation.

  • Czech name

  • Czech description

Classification

  • Type

    D - Article in proceedings

  • CEP classification

  • OECD FORD branch

    20505 - Composites (including laminates, reinforced plastics, cermets, combined natural and synthetic fibre fabrics; filled composites)

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

    2019

  • 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 proceedings

  • ISBN

    978-80-214-5696-9

  • ISSN

  • e-ISSN

  • Number of pages

    8

  • Pages from-to

    7-14

  • Publisher name

    VUT v Brně, Fakulta strojního inženýrství

  • Place of publication

    Brno

  • Event location

    Brno

  • Event date

    Nov 7, 2018

  • Type of event by nationality

    WRD - Celosvětová akce

  • UT code for WoS article

    000460498600001