About: Calculated and Measured Strength of a Composite Aircraft Undercarriage Spar

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

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rdf:type	skos:Concept http://linked.opendata.cz/ontology/domain/vavai/Vysledek
Description	The main aircraft undercarriage spar was designed using various criteria for laminate strength. The calculated stress-strain status was evaluated simultaneously with the use of basic phenomenological and mechanistic criteria for the set operating modes and the requested safety factors. Subsequently, prototypes of the spar were manufactured and subjected to structural tests. The obtained results provide important information concerning the reliability of the employed criteria in terms of prediction of the point of critical damage and the level of the corresponding load when applied on an actual aircraft component featuring a general reinforcement structure. The main aircraft undercarriage spar was designed using various criteria for laminate strength. The calculated stress-strain status was evaluated simultaneously with the use of basic phenomenological and mechanistic criteria for the set operating modes and the requested safety factors. Subsequently, prototypes of the spar were manufactured and subjected to structural tests. The obtained results provide important information concerning the reliability of the employed criteria in terms of prediction of the point of critical damage and the level of the corresponding load when applied on an actual aircraft component featuring a general reinforcement structure. (en)
Title	Calculated and Measured Strength of a Composite Aircraft Undercarriage Spar Calculated and Measured Strength of a Composite Aircraft Undercarriage Spar (en)
skos:prefLabel	Calculated and Measured Strength of a Composite Aircraft Undercarriage Spar Calculated and Measured Strength of a Composite Aircraft Undercarriage Spar (en)
skos:notation	RIV/00010669:_____/10:#0001070!RIV11-MSM-00010669
http://linked.open...avai/riv/aktivita	Z
http://linked.open...avai/riv/aktivity	Z(MSM0001066904)
http://linked.open...iv/cisloPeriodika	21
http://linked.open...vai/riv/dodaniDat	2011
http://linked.open...aciTvurceVysledku	Pompe, Vilém
http://linked.open.../riv/druhVysledku	J - Článek v odborném periodiku
http://linked.open...iv/duvernostUdaju	S - Úplné a pravdivé údaje nepodléhající ochraně podle zvláštních právních předpisů
http://linked.open...titaPredkladatele	Výzkumný a zkušební letecký ústav, a.s.
http://linked.open...dnocenehoVysledku	249474
http://linked.open...ai/riv/idVysledku	RIV/00010669:_____/10:#0001070
http://linked.open...riv/jazykVysledku	eng - angličtina
http://linked.open.../riv/klicovaSlova	composite; spar; failure; criterion; aircraft (en)
http://linked.open.../riv/klicoveSlovo	composite aircraft spar failure criterion
http://linked.open...odStatuVydavatele	CZ - Česká republika
http://linked.open...ontrolniKodProRIV	[C408B22C877B]
http://linked.open...i/riv/nazevZdroje	Bulletin of Applied Mechanics
http://linked.open...in/vavai/riv/obor	JI
http://linked.open...ichTvurcuVysledku	1 (xsd:int)
http://linked.open...cetTvurcuVysledku	1 (xsd:int)
http://linked.open...UplatneniVysledku	2010
http://linked.open...v/svazekPeriodika	6/2010
http://linked.open...iv/tvurceVysledku	Pompe, Vilém
http://linked.open...n/vavai/riv/zamer	Research in behaviour of composite materials in the primary structure of devices based on the principle of rotating lifting surface
issn	1801-1217
number of pages	4 (xsd:int)
is http://linked.open...avai/riv/vysledek of	Calculated and Measured Strength of a Composite Aircraft Undercarriage Spar Calculated and Measured Strength of a Composite Aircraft Undercarriage Spar Calculated and Measured Strength of a Composite Aircraft Undercarriage Spar

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