About: 3D Fabric Application on Glider Structures

Facets (new session)
Description
Metadata
Settings
- owl:sameAs
- Inference Rule:

About: 3D Fabric Application on Glider Structures Goto Sponge NotDistinct Permalink

An Entity of Type : http://linked.opendata.cz/ontology/domain/vavai/Vysledek, within Data Space : linked.opendata.cz associated with source document(s)

Attributes	Values
rdf:type	skos:Concept http://linked.opendata.cz/ontology/domain/vavai/Vysledek
Description	A material, called the Paraglass, has been used for the design of the ultralight composite glider, as a substitute for foam at sandwich structure. The material is used as middle lay of all coverings, which are the skin of wing, the fuselage and the tailplane. The advantage of this material is very simple and cheap technology of the structure production. The disadvantage is its weight and density. Before putting into production of aircraft, basic material tests were done to determinate tensile strength aand shear behaviour. The test results confirmed behaviour like isotropic panel. On the basis of results of initial tests and analyses, the lamination of the wing skin and fuselage was designed. Both wing and fuselage were tested and they provided the ability to carry ultimate loads. A material, called the Paraglass, has been used for the design of the ultralight composite glider, as a substitute for foam at sandwich structure. The material is used as middle lay of all coverings, which are the skin of wing, the fuselage and the tailplane. The advantage of this material is very simple and cheap technology of the structure production. The disadvantage is its weight and density. Before putting into production of aircraft, basic material tests were done to determinate tensile strength aand shear behaviour. The test results confirmed behaviour like isotropic panel. On the basis of results of initial tests and analyses, the lamination of the wing skin and fuselage was designed. Both wing and fuselage were tested and they provided the ability to carry ultimate loads. (en) A material, called the Paraglass, has been used for the design of the ultralight composite glider, as a substitute for foam at sandwich structure. The material is used as middle lay of all coverings, which are the skin of wing, the fuselage and the tailplane. The advantage of this material is very simple and cheap technology of the structure production. The disadvantage is its weight and density. Before putting into production of aircraft, basic material tests were done to determinate tensile strength aand shear behaviour. The test results confirmed behaviour like isotropic panel. On the basis of results of initial tests and analyses, the lamination of the wing skin and fuselage was designed. Both wing and fuselage were tested and they provided the ability to carry ultimate loads. (cs)
Title	3D Fabric Application on Glider Structures Aplikace 3D tkanin na kompozitní konstrukci kluzáku. (cs) 3D Fabric Application on Glider Structures (en)
skos:prefLabel	3D Fabric Application on Glider Structures Aplikace 3D tkanin na kompozitní konstrukci kluzáku. (cs) 3D Fabric Application on Glider Structures (en)
skos:notation	RIV/00216305:26210/05:PU48119!RIV06-MSM-26210___
http://linked.open.../vavai/riv/strany	1-100
http://linked.open...avai/riv/aktivita	P
http://linked.open...avai/riv/aktivity	P(1M0501)
http://linked.open...vai/riv/dodaniDat	2006
http://linked.open...aciTvurceVysledku	Juračka, Jaroslav
http://linked.open.../riv/druhVysledku	D - Článek ve sborníku
http://linked.open...iv/duvernostUdaju	S - Úplné a pravdivé údaje nepodléhající ochraně podle zvláštních právních předpisů
http://linked.open...titaPredkladatele	Vysoké učení technické v Brně / Fakulta strojního inženýrství
http://linked.open...dnocenehoVysledku	552726
http://linked.open...ai/riv/idVysledku	RIV/00216305:26210/05:PU48119
http://linked.open...riv/jazykVysledku	eng - angličtina
http://linked.open.../riv/klicovaSlova	parabeam, paraglass, form, 3D, share test, composite material (en)
http://linked.open.../riv/klicoveSlovo	form 3D composite material paraglass parabeam share test
http://linked.open...ontrolniKodProRIV	[7D25CF5413A7]
http://linked.open...v/mistoKonaniAkce	Melbourne
http://linked.open...i/riv/mistoVydani	Melbourne, Austálie
http://linked.open...i/riv/nazevZdroje	CD-Rom of Congress proceedings
http://linked.open...in/vavai/riv/obor	JU
http://linked.open...ichTvurcuVysledku	1 (xsd:int)
http://linked.open...cetTvurcuVysledku	1 (xsd:int)
http://linked.open...vavai/riv/projekt	Aerospace Research Centre
http://linked.open...UplatneniVysledku	2005
http://linked.open...iv/tvurceVysledku	Juračka, Jaroslav
http://linked.open...vavai/riv/typAkce	WRD - Světová
http://linked.open.../riv/zahajeniAkce	2005-03-13 (xsd:date)
number of pages	100 (xsd:int)
http://purl.org/ne...btex#hasPublisher	The Royal Aeronautical Society, Australia
https://schema.org/isbn	0-85825-732-7
http://localhost/t...ganizacniJednotka	26210

Faceted Search & Find service v1.16.118 as of Jun 21 2024

Alternative Linked Data Documents: ODE Content Formats:

RDF

ODATA

Microdata

About

OpenLink Virtuoso version 07.20.3240 as of Jun 21 2024, on Linux (x86_64-pc-linux-gnu), Single-Server Edition (126 GB total memory, 77 GB memory in use)
Data on this page belongs to its respective rights holders.
Virtuoso Faceted Browser Copyright © 2009-2024 OpenLink Software