In this paper we present an expert system to perform steady-state response predictions. We consider an aeroelastic model simulating a two degree-of-freedom airfoil oscillating in pitch and plunge with a freeplay nonlinearity in the pitch degreeof-freedom. In the proposed data-driven methodology, a f
โฆ LIBER โฆ
Equivalent damping of aeroelastic system of an airfoil with cubic stiffness
โ Scribed by Y.M. Chen; J.K. Liu; G. Meng
- Book ID
- 113711764
- Publisher
- Elsevier Science
- Year
- 2011
- Tongue
- English
- Weight
- 596 KB
- Volume
- 27
- Category
- Article
- ISSN
- 0889-9746
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