A combined parameter for graphic evaluation of the load capacity of fuselage
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F18%3APU128710" target="_blank" >RIV/00216305:26210/18:PU128710 - isvavai.cz</a>
Result on the web
<a href="https://www.crcpress.com/New-Trends-in-Civil-Aviation-Proceedings-of-the-19th-International-Conference/Socha-Hanakova-Lalis/p/book/9780815376026" target="_blank" >https://www.crcpress.com/New-Trends-in-Civil-Aviation-Proceedings-of-the-19th-International-Conference/Socha-Hanakova-Lalis/p/book/9780815376026</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1201/9781351238649" target="_blank" >10.1201/9781351238649</a>
Alternative languages
Result language
angličtina
Original language name
A combined parameter for graphic evaluation of the load capacity of fuselage
Original language description
Proper determination of the total load capacity of semi-monocoque structures without significant structural elements is a complex problem, which results in weight reduction of the designed structure. One critical failure can start the avalanche propagation of following failures and cause the total collapse of the structure. A typical example is a fuselage structure, which is stiffened by longitudinal stringers with similar shape and cross-section area. Therefore, in this study, we present a design and research of new specific combined parameters for faster determination of the load capacity of metal thin-walled semi-monocoque structures. The graphic visualization and evaluation of the avalanche propagation start is a post-processing method for determining a load capacity based on the results of analytical methods. New parameters were tested to evaluate the typical fuselage sections of a small transport aircraft in the CS-23 regulation category and to effectively determine the total load capacity of the fuselage structure.
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
CEP classification
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OECD FORD branch
20304 - Aerospace engineering
Result continuities
Project
<a href="/en/project/TE02000032" target="_blank" >TE02000032: Advanced Aerostructures Research Centre</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)
Others
Publication year
2018
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
New Trends in Civil Aviation
ISBN
978-0-8153-7602-6
ISSN
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e-ISSN
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Number of pages
5
Pages from-to
171-175
Publisher name
CRC Press
Place of publication
London, UK
Event location
Department of Air Transport, Czech Technical Uni
Event date
Dec 7, 2017
Type of event by nationality
EUR - Evropská akce
UT code for WoS article
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