Publication detail
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.
English title
Effect of angle of attack, gas composition and reynolds number on flutter boundary of benchmark super-critical wing
Type
conference paper
Language
en
Original abstract
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.
English abstract
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.
Keywords in English
AePW, Aeroelasticity, BSCW, Computational, Dynamics, Fluid,Flutter, Transonic
Released
01.05.2018
Publisher
Elsevier B.V.
ISBN
9788897576280
Book
17th International Forum on Aeroelasticity and Structural Dynamics, IFASD 2017
Pages from–to
1–10
Pages count
10
BIBTEX
@inproceedings{BUT149106,
author="Jan {Navrátil},
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",
month="May",
pages="1--10",
publisher="Elsevier B.V.",
isbn="9788897576280"
}