Publication detail

Computational Fluid Dynamics Study of Benchmark Supercritical Wing at Flutter Condition

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

Original Title

Computational Fluid Dynamics Study of Benchmark Supercritical Wing at Flutter Condition

Type

journal article in Web of Science

Language

English

Original Abstract

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.

Keywords

aeroelasticity, flutter, cfd, wing

Authors

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

Released

30. 8. 2016

Publisher

American Institute of Aeronautics and Astronautics, Inc.

ISBN

0001-1452

Periodical

AIAA JOURNAL

State

United States of America

Pages from

1

Pages to

8

Pages count

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"
}