Multidisciplinary design of aircraft wing for multiregime purposes
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F22%3AN0000077" target="_blank" >RIV/00010669:_____/22:N0000077 - isvavai.cz</a>
Result on the web
<a href="https://iopscience.iop.org/article/10.1088/1742-6596/2526/1/012002" target="_blank" >https://iopscience.iop.org/article/10.1088/1742-6596/2526/1/012002</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1088/1742-6596/2526/1/012002" target="_blank" >10.1088/1742-6596/2526/1/012002</a>
Alternative languages
Result language
angličtina
Original language name
Multidisciplinary design of aircraft wing for multiregime purposes
Original language description
In this paper optimization process of the geometrical design of the wing is described. The goal is to minimize the aerodynamic drag at a requested lift in the cruise regime and thus reduce the fuel consumption. The second goal is to ensure the requested landing regime of the aircraft. Both casesare solved under the wing structural and weight considerations. As a fast design computational tool, a lifting line theory is used. It is moreover supplemented by non-linear aerodynamic airfoil characteristics to provide more accurate results of aerodynamic drag of the wing. These airfoil data were calculated with the CFD and enables to take significant accuracy between low and high-fidelity method which is verified in previous work. The list of requirements is set for aircraft for 40 passengers with a range of 2,500 km at a speed of 438 km/h. As the baseline the L-610 aircraft is selected. Optimized wing geometry in verified in cruise and landing regime/configuration with CFD solver. From the calculation of the weight of the wing and CFD results, the flight performance is calculated for the desired flight mission.
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
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Continuities
I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace
Others
Publication year
2022
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
Journal of Physics: Conference Series
ISBN
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ISSN
17426588
e-ISSN
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Number of pages
8
Pages from-to
nestrankovano
Publisher name
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Place of publication
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Event location
Barcelona
Event date
Oct 21, 2022
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
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