The buckling in compression of panels with square top-hat section stringers
| dc.contributor.author | Hemp, W. S. | |
| dc.contributor.author | Griffin, K. H. | |
| dc.date.accessioned | 2012-05-15T14:48:26Z | |
| dc.date.available | 2012-05-15T14:48:26Z | |
| dc.date.issued | 1949-06 | |
| dc.description.abstract | A simplified panel model is described, together with a number of assumptions about the mode of its bucking. The approach to the calculation of the buckling stress is by splitting the panel into a number of flat plates and treating these by the ordinary plate theory. Use of the boundary conditions between these plates leads to a relation between the buckling stress and the variables of the panel geometry. The results thus obtained are compared with two sets of recent experimental work; and an appendix is included to show the effect of initial panel irregularities on the experimental determination of buckling stresses. | en_UK |
| dc.identifier.uri | http://dspace.lib.cranfield.ac.uk/handle/1826/7154 | |
| dc.language.iso | en | en_UK |
| dc.publisher | College of Aeronautics, Cranfield | en_UK |
| dc.relation.ispartofseries | College Report | en_UK |
| dc.relation.ispartofseries | 29 | en_UK |
| dc.title | The buckling in compression of panels with square top-hat section stringers | en_UK |
| dc.type | Report | en_UK |