Transonic flutter analysis of an AGARD 445.6 wing in the frequency domain using the Euler method

Transonic flutter analysis of an AGARD 445.6 wing in the frequency domain using the Euler method

A method based on the Euler equations is proposed for solving transonic flutter problems. The transonic nonlinear flow field with local shock wave/boundary layer interaction is obtained by the Euler/boundary layer equations, and the aerodynamic forces are converted from the time domain to the freque...

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Bibliographic Details
Main Authors: Bocheng Zhang, Weilong Ding, Shengcheng Ji, Jiazhen Zhang
Format: Article
Language:English
Published: Taylor & Francis Group 2016-01-01
Series:Engineering Applications of Computational Fluid Mechanics
Subjects:
Aeroelasticity
flutter
Euler equations
CFD/CSD
transonic flow
Online Access:http://dx.doi.org/10.1080/19942060.2016.1152200

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