Vibration and Aeroelasticity of Advanced Aircraft Wings Modeled as Thin-Walled Beams--Dynamics, Stability and Control
Based on a refined analytical anisotropic thin-walled beam model, aeroelastic instability, dynamic aeroelastic response, active/passive aeroelastic control of advanced aircraft wings modeled as thin-walled beams are systematically addressed. The refined thin-walled beam model is based on an existing...
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Virginia Tech
2014
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| Online Access: | http://hdl.handle.net/10919/29283 http://scholar.lib.vt.edu/theses/available/etd-10162001-114529/ |