Load diffusion at an interspar opening theoretical methods of analysis compared with strain measurements on a large wing

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dc.contributor.author D. C. Allen en_US
dc.date.accessioned 2014-10-21T15:52:14Z
dc.date.available 2014-10-21T15:52:14Z
dc.date.issued 1948 en_US
dc.identifier.other ARC/R&M-2664 en_US
dc.identifier.uri https://reports.aerade.cranfield.ac.uk/handle/1826.2/3205
dc.description.abstract The diffusion of load from spar flanges into skin and stringers near an opening was investigated experimentally in a large wing structure undergoing strength tests. A comparison of measured strains with those given by theoretical methods shows that in general the flange loads are represented with reasonable accuracy. Any theory, however, in which the chordwise rib at the edge of the opening is ignored gives shear stresses much greater than those measured. Allowance for the bending stiffness of this rib produces values of shear stress comparable with those obtained experimentally. en_US
dc.relation.ispartofseries Aeronautical Research Council Reports & Memoranda en_US
dc.title Load diffusion at an interspar opening theoretical methods of analysis compared with strain measurements on a large wing en_US


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