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Dubnický L., Šplíchal J., Juračka J.
Original Title
Sailplane wing sectioning based on structural weight
Type
article in a collection out of WoS and Scopus
Language
English
Original Abstract
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.
Keywords
Sailplane, Glider, Wing, Sectioning, Weight
Authors
Released
9. 5. 2023
Publisher
Institute of Thermomechanics of the Czech Academy of Sciences
Location
Praha
ISBN
978-80-87012-84-0
Book
Engineering Mechanics 2023, 29th International Conference
1805-8256
Periodical
Engineering Mechanics ....
Year of study
29
Number
1
State
Czech Republic
Pages from
59
Pages to
62
Pages count
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" }