dc.contributor.author |
E. H. Mansfield |
en_US |
dc.date.accessioned |
2014-10-21T15:53:04Z |
|
dc.date.available |
2014-10-21T15:53:04Z |
|
dc.date.issued |
1951 |
en_US |
dc.identifier.other |
ARC/R&M-2823 |
en_US |
dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/3378 |
|
dc.description.abstract |
The stress concentrations are determined for a panel, bounded by main load-carrying members and an oblique edge, such as might occur at a cut-out in a swept wing. The solutions given are exact and cover the effects of a member along the oblique edge and of closely-spaced stringers attached to the panel. |
en_US |
dc.relation.ispartofseries |
Aeronautical Research Council Reports & Memoranda |
en_US |
dc.title |
Stress concentrations at a cut-out in a swept wing |
en_US |