Flight by Flight Fatigue Test with Random Application of Loads

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F03%3APU38754" target="_blank" >RIV/00216305:26210/03:PU38754 - isvavai.cz</a>

Result on the web

—

DOI - Digital Object Identifier

—

Result language

angličtina

Original language name

Flight by Flight Fatigue Test with Random Application of Loads

Original language description

The most realistic method of experimental determining the mean fatigue life of an aircraft structure is a random application of loads on a flight by flight basis. This paper deals with the development of such load sequence which simulates a load historyas it can occur in service. A computer program was written for generation of load sequence. Calculations were also performed for the determination of the influence the small amplitude cycles omission on propagation of cracks in the spar web and wing skinn. Practical example of the wing spar specimen fatigue test using created load sequence is presented.

Czech name

—

Czech description

—

Type

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

CEP classification

JL - Fatigue and fracture mechanics

OECD FORD branch

—

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

Name of the periodical

Letecký zpravodaj

ISSN

1211-877X

e-ISSN

—

Volume of the periodical

2003

Issue of the periodical within the volume

3

Country of publishing house

CZ - CZECH REPUBLIC

Number of pages

4

Pages from-to

3-6

UT code for WoS article

—

EID of the result in the Scopus database

—