Dynamic aeroelasticity of aircraft with swept wings
Abstract
Using oblique coordinates, integro-differential equations of motion of aircraft with swept wings are deduced from Hamilton’s Principle for the dynamic problems of aero-elasticity, i.e. for the problems of free vibrations, flutter, dynamic stability and gust loadsSimilar works
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Last time updated on 20/03/2013
This paper was published in Cranfield CERES.
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