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Dubnický L., Šplíchal J., Juračka J.
Originální název
Sailplane wing sectioning based on structural weight
Typ
článek ve sborníku mimo WoS a Scopus
Jazyk
angličtina
Originální abstrakt
High-performance sailplanes use large wingspans, and the wings are split into sections to allow ground transport, storing and maintenance. Sometimes more section variants are available, resulting in different overall sailplane wingspans. Regular wing sectioning nowadays consists of 4 sections, with considerable weight differences between the inner and the outer sections. The option to use 3-piece sectioning is reviewed and combined with 2 wingspan variants. The splitting location, based on the equal weight distribution among the sections, is calculated according to the wing weight distribution model. The following structural design provided a more accurate wing mass value and the weight distribution model. The original and the calculated weight distributions are compared and an improvement is suggested for later application.
Klíčová slova
Sailplane, Glider, Wing, Sectioning, Weight
Autoři
Vydáno
9. 5. 2023
Nakladatel
Institute of Thermomechanics of the Czech Academy of Sciences
Místo
Praha
ISBN
978-80-87012-84-0
Kniha
Engineering Mechanics 2023, 29th International Conference
ISSN
1805-8256
Periodikum
Engineering Mechanics ....
Ročník
29
Číslo
1
Stát
Česká republika
Strany od
59
Strany do
62
Strany počet
4
URL
https://www.engmech.cz/improc/2023/059.pdf
BibTex
@inproceedings{BUT187746, author="Lukáš {Dubnický} and Jan {Šplíchal} and Jaroslav {Juračka}", title="Sailplane wing sectioning based on structural weight", booktitle="Engineering Mechanics 2023, 29th International Conference", year="2023", journal="Engineering Mechanics ....", volume="29", number="1", pages="59--62", publisher="Institute of Thermomechanics of the Czech Academy of Sciences", address="Praha", doi="10.21495/em2023-59", isbn="978-80-87012-84-0", issn="1805-8256", url="https://www.engmech.cz/improc/2023/059.pdf" }