Detail publikace

Effect of angle of attack, gas composition and reynolds number on flutter boundary of benchmark super-critical wing

NAVRÁTIL, J. JIRÁSEK, A. HAMLINGTON, P. LOFTHOUSE, A.

Originální název

Effect of angle of attack, gas composition and reynolds number on flutter boundary of benchmark super-critical wing

Typ

článek ve sborníku ve WoS nebo Scopus

Jazyk

angličtina

Originální abstrakt

This paper presents results of the second Aeroelastic Prediction Workshop which uses the Benchmark Super-Critical Wing, BSCW at flutter conditions as a common test case. The primary purpose of this study is to evaluate the effect of angle of attack. To do so, we analyzed BSCW wing at three angles of attack - α = 0deg, α = 1deg and α = 5deg. The second task is to evaluate the effect of gas composition on flutter boundary. The two gases are R-12 heavy gas, used as a test medium for the wind tunnel test, and air.

Klíčová slova

AePW, Aeroelasticity, BSCW, Computational, Dynamics, Fluid,Flutter, Transonic

Autoři

NAVRÁTIL, J.; JIRÁSEK, A.; HAMLINGTON, P.; LOFTHOUSE, A.

Vydáno

1. 5. 2018

Nakladatel

Elsevier B.V.

ISBN

9788897576280

Kniha

17th International Forum on Aeroelasticity and Structural Dynamics, IFASD 2017

Strany od

1

Strany do

10

Strany počet

10

BibTex

@inproceedings{BUT149106,
  author="NAVRÁTIL, J. and JIRÁSEK, A. and HAMLINGTON, P. and LOFTHOUSE, A.",
  title="Effect of angle of attack, gas composition and reynolds number on flutter boundary of benchmark super-critical wing",
  booktitle="17th International Forum on Aeroelasticity and Structural Dynamics, IFASD 2017",
  year="2018",
  pages="1--10",
  publisher="Elsevier B.V.",
  isbn="9788897576280"
}