Coiley, G. H.2012-09-132012-09-131954-03http://dspace.lib.cranfield.ac.uk/handle/1826/7580A theoretical solutions for stress concentrations as might occur in a swept wing, has benn derived by E.H. Mansfield. This thesis applies photoelastic techniques to models of wing panels with various angles of sweep, with object of verifying these equations.enReport