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Detail publikačního výsledku
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
Anglický název
Druh
Stať ve sborníku v databázi WoS či Scopus
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.
Anglický abstrakt
Klíčová slova
AePW, Aeroelasticity, BSCW, Computational, Dynamics, Fluid,Flutter, Transonic
Klíčová slova v angličtině
Autoři
Rok RIV
2019
Vydáno
01.05.2018
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
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" }