Detail publikace

Aerodynamic shape optimization of an airliner elastic wing

NAVRÁTIL, J.

Originální název

Aerodynamic shape optimization of an airliner elastic wing

Typ

článek ve sborníku ve WoS nebo Scopus

Jazyk

angličtina

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.

Klíčová slova

aerodynamic, shape, optimization, elastic, transonic, wing

Autoři

NAVRÁTIL, J.

Vydáno

8. 11. 2017

Nakladatel

EDP Sciences

Místo

Francie

ISBN

9781510851924

Kniha

12th International Conference on Applied Mathematical Programming and Modelling (APMOD 2016)

ISSN

2271-2097

Periodikum

ITM Web of Conferences

Ročník

14

Číslo

00006

Stát

Francouzská republika

Strany od

1

Strany do

9

Strany počet

9

URL

https://www.itm-conferences.org/articles/itmconf/abs/2017/06/itmconf_apmod2017_00006/itmconf_apmod2017_00006.html

Plný text v Digitální knihovně

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"
}