Experimental Investigation of Composite Material Propeties of Aircraft Structures

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F03%3A02091409" target="_blank" >RIV/68407700:21220/03:02091409 - 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

Experimental Investigation of Composite Material Propeties of Aircraft Structures

Original language description

Material characteristics investigation of composite materials used at design of light and very light aeroplanes. Rising Composite Material Database contains material properties, measured composite material and engineering characteristics, material components tests, description and philosophy of experiments, specimen technological processing and notation key. Tested materials are composite materials with glass, carbon or carbon-aramid reinforcement and epoxy matrix used for building light and very lightaeroplanes, produced by contact lamination. The orientation of specimen reinforcers with respect to load direction is 0°, 45° and 90°. There is considered static tensile test, pressure, bend test, shear and interlaminar shear test. All static experimentsare provided at temperatures 23°C, 54°C, -55°C and 23°C with increased moisture.

Czech name

Není k dispozici

Czech description

Není k dispozici

Type

A - Audiovisual production

CEP classification

JI - Composite materials

OECD FORD branch

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Project

<a href="/en/project/LN00B051" target="_blank" >LN00B051: Aerospace research centre (ARC)</a><br>

Continuities

P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Publication year

2003

Confidentiality

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

ISBN

80-01-02708-2

Place of publication

Praha

Publisher/client name

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Version

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Carrier ID

neuvedeno