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|Document Type: ||Report|
|Title: ||The buckling in compression of panels with square top-hat section stringers|
|Authors: ||Hemp, W. S.|
Griffin, K. H.
|Issue Date: ||Jun-1949|
|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.|
|Appears in Collections:||College of Aeronautics Reports|
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