Calculated and Measured Strength of a Composite Aircraft Undercarriage Spar

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F10%3A%230001070" target="_blank" >RIV/00010669:_____/10:#0001070 - isvavai.cz</a>

Výsledek na webu

—

DOI - Digital Object Identifier

—

Jazyk výsledku

angličtina

Název v původním jazyce

Calculated and Measured Strength of a Composite Aircraft Undercarriage Spar

Popis výsledku v původním jazyce

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.

Název v anglickém jazyce

Calculated and Measured Strength of a Composite Aircraft Undercarriage Spar

Popis výsledku anglicky

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.

Druh

J_x - Nezařazeno - Článek v odborném periodiku (Jimp, Jsc a Jost)

CEP obor

JI - Kompositní materiály

OECD FORD obor

—

Projekt

—

Návaznosti

Z - Vyzkumny zamer (s odkazem do CEZ)

Rok uplatnění

2010

Kód důvěrnosti údajů

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

Název periodika

Bulletin of Applied Mechanics

ISSN

1801-1217

e-ISSN

—

Svazek periodika

6/2010

Číslo periodika v rámci svazku

21

Stát vydavatele periodika

CZ - Česká republika

Počet stran výsledku

4

Strana od-do

—

Kód UT WoS článku

—

EID výsledku v databázi Scopus

—