Detail publikace
Aerodynamic shape optimization of an airliner elastic wing
NAVRÁTIL, J.
Anglický název
Aerodynamic shape optimization of an airliner elastic wing
Typ
článek ve sborníku ve WoS nebo Scopus
Jazyk
en
Originální abstrakt
Aerodynamic shape optimization of a common airliner elastic wing is presented and compared with optimization of the same wing assuming rigid structure. A gradient-based optimization approach is applied in connection with adjoint method used for calculation of gradients of aerodynamic forces. The initial wing shape is parameterized by Free Form Deformation technique. The aerodynamics of the elastic wing is calculated using the fluid-structure interaction method which couples computational fluid dynamic solver with linear structural solver.
Anglický abstrakt
Aerodynamic shape optimization of a common airliner elastic wing is presented and compared with optimization of the same wing assuming rigid structure. A gradient-based optimization approach is applied in connection with adjoint method used for calculation of gradients of aerodynamic forces. The initial wing shape is parameterized by Free Form Deformation technique. The aerodynamics of the elastic wing is calculated using the fluid-structure interaction method which couples computational fluid dynamic solver with linear structural solver.
Klíčová slova anglicky
aerodynamic, shape, optimization, elastic, transonic, wing
Vydáno
08.11.2017
Nakladatel
EDP Sciences
Místo
Francie
ISBN
9781510851924
ISSN
2271-2097
Kniha
12th International Conference on Applied Mathematical Programming and Modelling (APMOD 2016)
Ročník
14
Číslo
00006
Strany od–do
1–9
Počet stran
9
BIBTEX
@inproceedings{BUT127580,
author="Jan {Navrátil},
title="Aerodynamic shape optimization of an airliner elastic wing",
booktitle="12th International Conference on Applied Mathematical Programming and Modelling (APMOD 2016) ",
year="2017",
volume="14",
number="00006",
month="November",
pages="1--9",
publisher="EDP Sciences",
address="Francie",
isbn="9781510851924",
issn="2271-2097"
}