Abstract
This paper presents experimental evidence of the transient growth of energy for the coupled-mode flutter of an airfoil. The phenomenon occurs even in linearly stable dynamical systems. Its application is new in the context of fluid-structure interactions where only theoretical and numerical studies of transient growth exist. The experimental set-up allows an NACA 0015 airfoil to oscillate in rotational and vertical degrees of freedom when it is subjected to air-flow. Measurements consist of time series of the two motions obtained by laser displacement sensors. Structural parameters are first estimated without air-flow. The transient evolution of energy is measured, and amplification is observed for a given set of initial conditions. Our experiments agree well with numerical simulations based on unsteady airfoil theory.
| Original language | English |
|---|---|
| Pages (from-to) | 391-400 |
| Number of pages | 10 |
| Journal | Journal of Fluids and Structures |
| Volume | 22 |
| Issue number | 3 |
| DOIs | |
| Publication status | Published - 1 Apr 2006 |
Keywords
- Flutter instability
- Transient growth
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