Publication detail

Computational Fluid Dynamics Study of Benchmark Supercritical Wing at Flutter Condition

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

English title

Computational Fluid Dynamics Study of Benchmark Supercritical Wing at Flutter Condition

Type

journal article in Web of Science

Language

en

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.

English 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 in English

aeroelasticity, flutter, cfd, wing

Released

30.08.2016

Publisher

American Institute of Aeronautics and Astronautics, Inc.

ISSN

0001-1452

Pages from–to

1–8

Pages count

8

BIBTEX


@article{BUT127568,
  author="Jan {Navrátil},
  title="Computational Fluid Dynamics Study of Benchmark Supercritical Wing at Flutter Condition",
  year="2016",
  month="August",
  pages="1--8",
  publisher="American Institute of Aeronautics and Astronautics, Inc.",
  issn="0001-1452"
}