In this paper single mode panel flutter, which occurs at low supersonic Mach numbers, is studied. Numerical analysis which does not require solution of coupled FSI problem has been conducted. Flutter boundaries obtained are compared with previously known analytical results.

Volume Subject Area:
7th International Symposium on Fluid-Structure Interactions, Flow-Sound Interactions, and Flow-Induced Vibration and Noise
Topics:
Flutter (Aerodynamics), Gas flow, Numerical analysis, Fluid structure interaction, Mach number
This content is only available via PDF.
Copyright © 2010
 by ASME
You do not currently have access to this content.