Stress concentration in swept wing panels using photoelastic models

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dc.contributor.authorCoiley, G. H.
dc.date.accessioned2012-09-13T15:38:53Z
dc.date.available2012-09-13T15:38:53Z
dc.date.issued1954-03
dc.description.abstractA 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.identifier.urihttp://dspace.lib.cranfield.ac.uk/handle/1826/7580
dc.language.isoenen_UK
dc.publisherCollege of Aeronautics, Cranfielden_UK
dc.relation.ispartofseriesCollege Reportsen_UK
dc.relation.ispartofseries78en_UK
dc.titleStress concentration in swept wing panels using photoelastic modelsen_UK
dc.typeReporten_UK

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