The buckling of a square panel under shear when one pair of opposite edges is clamped, and the other pair is simply supported

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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


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