Nonlinear behavior of foam material

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F12%3APU100604" target="_blank" >RIV/00216305:26210/12:PU100604 - isvavai.cz</a>

Result on the web

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DOI - Digital Object Identifier

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Result language

angličtina

Original language name

Nonlinear behavior of foam material

Original language description

Nowadays, composite materials are often used in aircraft structures. The most common construction is sandwich structure. Very important part of sandwich structure is core material. For core material can be used honeycomb or foam. In our tests herex foammaterial was used. The following article presents the results of experimental tests to determine nonlinear behavior of herex foam. Compression tests were done for finding module of elasticity and compression strength. Shear tests were done for finding shear modulus and ultimate shear stress. Consequently was performed verification finite elements analysis. This data can be used for design of sandwich structure and its load capability.

Czech name

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Czech description

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Type

J_x - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)

CEP classification

JU - Aeronautics, aerodynamics, aeroplanes

OECD FORD branch

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Project

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Continuities

S - Specificky vyzkum na vysokych skolach

Publication year

2012

Confidentiality

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Name of the periodical

RESEARCH BULLETIN

ISSN

1425-2104

e-ISSN

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Volume of the periodical

2012

Issue of the periodical within the volume

22

Country of publishing house

PL - POLAND

Number of pages

9

Pages from-to

1-9

UT code for WoS article

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EID of the result in the Scopus database

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