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KATRŇÁK, T.
Original Title
A combined parameter for graphic evaluation of the load capacity of fuselage
Type
lecture
Language
English
Original Abstract
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.
Keywords
load capacity, fuselage, semi-monocoque, stress analysis, failure
Authors
Released
7. 12. 2017
Publisher
CRC Press
Location
London, UK
Pages from
171
Pages to
175
Pages count
5
URL
https://www.crcpress.com/New-Trends-in-Civil-Aviation-Proceedings-of-the-19th-International-Conference/Socha-Hanakova-Lalis/p/book/9780815376026
BibTex
@misc{BUT146193, author="Tomáš {Katrňák}", title="A combined parameter for graphic evaluation of the load capacity of fuselage", year="2017", pages="171--175", publisher="CRC Press", address="London, UK", url="https://www.crcpress.com/New-Trends-in-Civil-Aviation-Proceedings-of-the-19th-International-Conference/Socha-Hanakova-Lalis/p/book/9780815376026", note="lecture" }