Stress concentration in swept wing panels using photoelastic models

Coiley, G. H.

dc.contributor.author	Coiley, G. H.
dc.date.accessioned	2012-09-13T15:38:53Z
dc.date.available	2012-09-13T15:38:53Z
dc.date.issued	1954-03
dc.identifier.uri	http://dspace.lib.cranfield.ac.uk/handle/1826/7580
dc.description.abstract	A 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.	en_UK
dc.language.iso	en	en_UK
dc.publisher	College of Aeronautics, Cranfield	en_UK
dc.relation.ispartofseries	College Reports	en_UK
dc.relation.ispartofseries	78	en_UK
dc.title	Stress concentration in swept wing panels using photoelastic models	en_UK
dc.type	Report	en_UK