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NAVRÁTIL, J.
Original Title
Aerodynamic shape optimization of an airliner elastic wing
English Title
Type
Paper in proceedings (conference paper)
Original Abstract
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.
English abstract
Keywords
aerodynamic, shape, optimization, elastic, transonic, wing
Key words in English
Authors
RIV year
2018
Released
08.11.2017
Publisher
EDP Sciences
Location
Francie
ISBN
9781510851924
Book
12th International Conference on Applied Mathematical Programming and Modelling (APMOD 2016)
2271-2097
Periodical
ITM Web of Conferences
Volume
14
Number
00006
State
French Republic
Pages from
1
Pages to
9
Pages count
URL
https://www.itm-conferences.org/articles/itmconf/abs/2017/06/itmconf_apmod2017_00006/itmconf_apmod2017_00006.html
Full text in the Digital Library
http://hdl.handle.net/11012/81243
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", journal="ITM Web of Conferences", volume="14", number="00006", pages="1--9", publisher="EDP Sciences", address="Francie", doi="10.1051/itmconf/20171400006", isbn="9781510851924", issn="2271-2097", url="https://www.itm-conferences.org/articles/itmconf/abs/2017/06/itmconf_apmod2017_00006/itmconf_apmod2017_00006.html" }
Documents
itmconf_apmod2017_00006