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.
Computational Fluid Dynamics Study of Benchmark Supercritical Wing at Flutter Condition
AIAA Journal ; 55 , 1 ; 153-160
2016-08-30
8 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Computational Fluid Dynamics Study of Benchmark Supercritical Wing at Flutter Condition
Online Contents | 2017
|Computational Fluid Dynamics Study of Benchmark Supercritical Wing at Flutter Condition
Online Contents | 2016
|NTIS | 1978
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