Detail publikace

Numerical Study of Benchmark Super-Critical Wing, BSCW, at Flutter Condition

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

Anglický název

Numerical Study of Benchmark Super-Critical Wing, BSCW, at Flutter Condition

Typ

článek ve sborníku ve WoS nebo Scopus

Jazyk

en

Originální abstrakt

This paper presents a numerical study of the Benchmark Super-Critical Wing, BSCW at flutter condition which were done as a part of the AIAA Aeroelastic Predictions Workshop, AePW II. The primary purpose is the evaluation of the time synchronization effect on the convergence of the coupled CFD-CSM process.

Anglický abstrakt

This paper presents a numerical study of the Benchmark Super-Critical Wing, BSCW at flutter condition which were done as a part of the AIAA Aeroelastic Predictions Workshop, AePW II. The primary purpose is the evaluation of the time synchronization effect on the convergence of the coupled CFD-CSM process.

Klíčová slova anglicky

flutter, aeroelasticity, numerical, transonic, wing

Vydáno

08.01.2016

Nakladatel

AIAA

ISBN

978-1-62410-393-3

Kniha

54th AIAA Aerospace Sciences Meeting

Strany od–do

1–11

Počet stran

11

BIBTEX


@inproceedings{BUT123265,
  author="Jan {Navrátil},
  title="Numerical Study of Benchmark Super-Critical Wing, BSCW, at Flutter Condition",
  booktitle="54th AIAA Aerospace Sciences Meeting",
  year="2016",
  month="January",
  pages="1--11",
  publisher="AIAA",
  isbn="978-1-62410-393-3"
}