Radok, J. R. M.2012-07-252012-07-251952-03http://dspace.lib.cranfield.ac.uk/handle/1826/7420Using oblique coordinates, the static problems of Aero-elasticity for swept wings are reduced to the solution of integral – or matrix equations, which may be solved by iteration. The present treatment also indicates the suitability of integral equations for fundamental aero-elastic investigations. Continues …enAileron reversal and divergence of swept wings with special consideration of the relevant aerodynamic and elastic characteristicsReport