Stress concentration in swept wing panels using photoelastic models

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dc.creator Coiley, G. H.
dc.date 2012-09-13T15:38:53Z
dc.date 2012-09-13T15:38:53Z
dc.date 1954-03
dc.date.accessioned 2022-05-09T10:17:21Z
dc.date.available 2022-05-09T10:17:21Z
dc.identifier http://dspace.lib.cranfield.ac.uk/handle/1826/7580
dc.identifier.uri https://reports.aerade.cranfield.ac.uk/handle/1826.2/4753
dc.description 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.
dc.language en
dc.publisher College of Aeronautics, Cranfield
dc.relation College Reports
dc.relation 78
dc.title Stress concentration in swept wing panels using photoelastic models
dc.type Report


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