dc.contributor.author |
D. M. A. Leggett |
|
dc.date.accessioned |
2014-10-21T12:03:31Z |
|
dc.date.available |
2014-10-21T12:03:31Z |
|
dc.date.issued |
1941 |
|
dc.identifier.other |
ARC/R&M-1991 |
en_US |
dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/1450 |
|
dc.description.abstract |
For an efficient design of spar with thin sheet web it is important to know the load which will just cause the web to buckle. As stiffeners divide the web into panels, it is required to find the buckling stress of rectangular panels bounded on two sides by spar flanges and on the other two sides by stiffeners. Boundary conditions which represent closely this type of edge fixing are clamping (along the flanges) and simple support (along the stiffeners), and the object of this report is to find the critical shear stress for a square panel held in this way. |
en_US |
dc.language.iso |
en |
en_US |
dc.publisher |
H. M. Stationery Office |
en_US |
dc.relation.ispartofseries |
Aeronautical Research Committee Reports & Memoranda |
en_US |
dc.title |
The buckling of a square panel under shear when one pair of opposite edges is clamped, and the other pair is simply supported |
en_US |
dc.type |
Technical Report |
en_US |