Multidisciplinary design of the wing for aircraft preliminary design purposes

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F20%3AN0000030" target="_blank" >RIV/00010669:_____/20:N0000030 - isvavai.cz</a>
Result on the web
<a href="https://iopscience.iop.org/article/10.1088/1757-899X/1024/1/012045/pdf" target="_blank" >https://iopscience.iop.org/article/10.1088/1757-899X/1024/1/012045/pdf</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1088/1757-899X/1024/1/012045" target="_blank" >10.1088/1757-899X/1024/1/012045</a>

Result language
angličtina
Original language name
Multidisciplinary design of the wing for aircraft preliminary design purposes
Original language description
In this paper, an aerodynamic and wing structure is investigated by low-fidelity methods. Bell-shaped lift distribution was rediscovered in the last decade as a perspective alternative to traditional wing design. This leads to lower aerodynamic drag than elliptical lift distribution for a given lift force and root bending moment.
Czech name
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Czech description
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Project
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Continuities
I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Publication year
2020
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
10th EASN International Conference on Innovation in Aviation & Space to the Satisfaction of the European Citizens (10th EASN 2020) 2nd-5th September 2020
ISBN
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ISSN
1757-8981
e-ISSN
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Number of pages
7
Pages from-to
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Publisher name
IOP Conference Series
Place of publication
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Event location
online
Event date
Sep 2, 2020
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
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