Radok, J. R. M.2012-07-262012-07-261952-04http://dspace.lib.cranfield.ac.uk/handle/1826/7432Using 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 loads.enReport