Aerodynamic Design and Strength Analysis of the Wing for the Purpose of Assessing the Influence of the Bell-Shaped Lift Distribution

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F21%3AN0000023" target="_blank" >RIV/00010669:_____/21:N0000023 - isvavai.cz</a>

Result on the web

<a href="https://www.mdpi.com/2226-4310/9/1/13" target="_blank" >https://www.mdpi.com/2226-4310/9/1/13</a>

DOI - Digital Object Identifier

<a href="http://dx.doi.org/10.3390/aerospace9010013" target="_blank" >10.3390/aerospace9010013</a>

Result language

angličtina

Original language name

Aerodynamic Design and Strength Analysis of the Wing for the Purpose of Assessing the Influence of the Bell-Shaped Lift Distribution

Original language description

This article deals with aerodynamic and structural calculations of several wing designs to compare the influence of the shape on the lift distribution. Various shapes of wings for the required lift and bending moment were optimized to minimize drag and thereby reduce fuel consumption. One example was a wing with a bell-shaped lift distribution, which was proposed by Ludwig Prandtl and has been forgotten over the years.

Czech name

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Czech description

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Type

J_imp - Article in a specialist periodical, which is included in the Web of Science database

CEP classification

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OECD FORD branch

20304 - Aerospace engineering

Project

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Continuities

I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Publication year

2021

Confidentiality

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Name of the periodical

Aerospace Journal

ISSN

2226-4310

e-ISSN

2226-4310

Volume of the periodical

9

Issue of the periodical within the volume

1

Country of publishing house

CH - SWITZERLAND

Number of pages

20

Pages from-to

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UT code for WoS article

000760437700001

EID of the result in the Scopus database

2-s2.0-85122250959