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- W2316090138 abstract "The prediction of flutter onset based on aerodynamic modelling using CFD can be made using an augmented system of equations. Computational times similar to those required for CFD steady state calculations have been reported for wing test cases. However, for such methods to be fully useful, information about damping must be obtainable without reverting to full order time domain simulation. This paper presents a method for computing damping based on a reduced order modelling approach which systematically derives a two degree of freedom model from the full discrete system of equations. The method is based on a change of variables which employs the critical eigenvector of the aeroelastic system. The ability of this model to predict the damping for a model problem and two wing test cases is shown." @default.
- W2316090138 created "2016-06-24" @default.
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- W2316090138 date "2006-05-01" @default.
- W2316090138 modified "2023-09-25" @default.
- W2316090138 title "A Reduced Order Model for Damping Derived from CFD Based Aeroelastic Simulations" @default.
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- W2316090138 doi "https://doi.org/10.2514/6.2006-2021" @default.
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