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Stress Distribution Investigation at the Tapered Sandwich Endings

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F18%3APU126697" target="_blank" >RIV/00216305:26210/18:PU126697 - isvavai.cz</a>

  • Result on the web

    <a href="http://ilot.edu.pl/eng_prace_ilot/?list_of_transactions/249_2017/5.html" target="_blank" >http://ilot.edu.pl/eng_prace_ilot/?list_of_transactions/249_2017/5.html</a>

  • DOI - Digital Object Identifier

Alternative languages

  • Result language

    angličtina

  • Original language name

    Stress Distribution Investigation at the Tapered Sandwich Endings

  • Original language description

    One of the typical sandwich ending is tapered transition to a solid laminate, which causes significant stress distribution changes. The reviewed articles show that tapered area causes increase in the shear stress in the core, increase of the axial forces in the facesheets and local bending at the fork point, points of the tapering angle change, and at ply drop positions. Most of the studies gave attention to the endings without reinforcing. During Erasmus+ internship at KTH 2D model of the tapered ending with reinforcing plies, various geometry and resin filler in the core tip was investigated to see the influence on the stress distribution. It was found that tension load case is not as critical as bending load case. Increasing of the solid laminate thickness, adding plies and inserting a short resin or adhesive filler into the core tip area lead to significant stress reduction, whereas in the transition point, from tapering to constant thickness sandwich, increasing radius is more efficient than reinforcing plies in regard to reduce stress concentration.

  • Czech name

  • Czech description

Classification

  • Type

    J<sub>ost</sub> - Miscellaneous article in a specialist periodical

  • CEP classification

  • OECD FORD branch

    20304 - Aerospace engineering

Result continuities

  • Project

    <a href="/en/project/ED0002%2F01%2F01" target="_blank" >ED0002/01/01: NETME Centre (New Technologies for Mechanical Engineering)</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

  • Name of the periodical

    Transactions of the Institute of Aviation

  • ISSN

    0509-6669

  • e-ISSN

  • Volume of the periodical

    2017

  • Issue of the periodical within the volume

    4(249)

  • Country of publishing house

    PL - POLAND

  • Number of pages

    18

  • Pages from-to

    62-79

  • UT code for WoS article

  • EID of the result in the Scopus database