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Experimental verification of jet engine composite inlet for bird and hail stone impact resistance

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F18%3AN0000060" target="_blank" >RIV/00010669:_____/18:N0000060 - isvavai.cz</a>

  • Result on the web

  • DOI - Digital Object Identifier

Alternative languages

  • Result language

    angličtina

  • Original language name

    Experimental verification of jet engine composite inlet for bird and hail stone impact resistance

  • Original language description

    Bird and hail strike is a major threat for aircraft structure, as it can lead to serious structural damage. The vulnerable parts of planes or helicopters are windshield, nose, fuselage panels, wing and empennage leading edges, rotor blades, fan blades and engines inlets. Therefore, the international certification regulation requires [1] all forward facing components to prove a certain level of bird strike resistance before they can be employed in an aircraft. A bird or hail impact experiment provides a direct method to examine the impact structure resistance. A simultaneous work between experiments and numerical simulations is necessary to well understand the behavior of a bird or hail during an impact and also the reaction of the impacted material and structure.

  • 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

    Experimental Stress Analysis - 56th International Scientific Conference, EAN 2018 - Conference Proceedings

  • ISBN

    978-80-270-4062-9

  • ISSN

  • e-ISSN

  • Number of pages

    14

  • Pages from-to

    63-76

  • Publisher name

    Czech Society for Mechanics

  • Place of publication

    Liberec

  • Event location

    Harrachov

  • Event date

    Jun 5, 2018

  • Type of event by nationality

    EUR - Evropská akce

  • UT code for WoS article