An Advanced Fatigue Strength Certification Method for Small Aircraft Thin-walled Primary Part

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F10%3A%230001026" target="_blank" >RIV/00010669:_____/10:#0001026 - 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

An Advanced Fatigue Strength Certification Method for Small Aircraft Thin-walled Primary Part

Original language description

The article gives short information about using an advanced fatigue strength certification method which is suitable for application to thin walled primary structural parts of small aircraft. Preparation and implementation procedures for fatigue testing of thin-walled wing structure of KP-5-ASA aircraft are used as a basis to develop a modern certification test methodology since they represent the fatigue life certification case of small aircraft´s primary structure in a model situation that faces most manufacturers during the development phase of this type of airplane.

Czech name

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Czech description

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Type

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

CEP classification

JL - Fatigue and fracture mechanics

OECD FORD branch

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Project

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Continuities

Z - Vyzkumny zamer (s odkazem do CEZ)

Publication year

2010

Confidentiality

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

Name of the periodical

Czech Aerospace Proceedings / Letecký zpravodaj

ISSN

1211-877X

e-ISSN

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Volume of the periodical

4/2010

Issue of the periodical within the volume

4

Country of publishing house

CZ - CZECH REPUBLIC

Number of pages

2

Pages from-to

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UT code for WoS article

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EID of the result in the Scopus database

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