SHAPE MODIFICATIONS OF CRITICAL FUSELAGE PARTS ACCORDING TO FATIGUE DURABILITY
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F12%3APU100365" target="_blank" >RIV/00216305:26210/12:PU100365 - isvavai.cz</a>
Result on the web
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DOI - Digital Object Identifier
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Alternative languages
Result language
angličtina
Original language name
SHAPE MODIFICATIONS OF CRITICAL FUSELAGE PARTS ACCORDING TO FATIGUE DURABILITY
Original language description
The article presents a shape optimization of critical fuselage wall segments and undercarriage spars, a localization of stress concentrations and modifications for a reduction and removing of stress peaks. Structural analyses are made on main fuselage parts on the aircraft in CS-23 Commuter category. There are described main types of proper shape modifications with graphic comparisons and highlighted stress peaks.
Czech name
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Czech description
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Classification
Type
J<sub>x</sub> - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)
CEP classification
JU - Aeronautics, aerodynamics, aeroplanes
OECD FORD branch
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Result continuities
Project
<a href="/en/project/FR-TI2%2F557" target="_blank" >FR-TI2/557: Project MOSTA - Modernization Of Small Transport Aircraft to increase operation effectiveness and economy</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)
Others
Publication year
2012
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Name of the periodical
RESEARCH BULLETIN
ISSN
1425-2104
e-ISSN
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Volume of the periodical
2012
Issue of the periodical within the volume
22
Country of publishing house
PL - POLAND
Number of pages
8
Pages from-to
1-8
UT code for WoS article
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EID of the result in the Scopus database
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