Detail publikace

Computational Fluid Dynamics Study of Benchmark Supercritical Wing at Flutter Condition

JIRÁSEK, A. NAVRÁTIL, J. DALENBRING, M.

Originální název

Computational Fluid Dynamics Study of Benchmark Supercritical Wing at Flutter Condition

Typ

článek v časopise ve Web of Science, Jimp

Jazyk

angličtina

Originální abstrakt

This paper presents a numerical study of the Benchmark Supercritical Wing at flutter condition, which was performed as a part of the AIAA Aeroelastic Prediction Workshop II. The primary purpose is the evaluation of the time-synchronization effect on the convergence of the coupled computational fluid dynamics/computational structural mechanics process. The proposed methodology was then used to predict the flutter boundary for the range of Mach numbers.

Klíčová slova

aeroelasticity, flutter, cfd, wing

Autoři

JIRÁSEK, A.; NAVRÁTIL, J.; DALENBRING, M.

Vydáno

30. 8. 2016

Nakladatel

American Institute of Aeronautics and Astronautics, Inc.

ISSN

0001-1452

Periodikum

AIAA JOURNAL

Stát

Spojené státy americké

Strany od

1

Strany do

8

Strany počet

8

URL

http://arc.aiaa.org/doi/10.2514/1.J054916

BibTex

@article{BUT127568,
  author="JIRÁSEK, A. and NAVRÁTIL, J. and DALENBRING, M.",
  title="Computational Fluid Dynamics Study of Benchmark Supercritical Wing at Flutter Condition",
  journal="AIAA JOURNAL",
  year="2016",
  volume="0",
  number="0",
  pages="1--8",
  doi="10.2514/1.J054916",
  issn="0001-1452",
  url="http://arc.aiaa.org/doi/10.2514/1.J054916"
}