Compression tests on dural-celluboard sandwich panels

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dc.contributor.author K. H. V. Britten en_US
dc.date.accessioned 2014-10-21T15:52:11Z
dc.date.available 2014-10-21T15:52:11Z
dc.date.issued 1946 en_US
dc.identifier.other ARC/R&M-2658 en_US
dc.identifier.uri https://reports.aerade.cranfield.ac.uk/handle/1826.2/3198
dc.description.abstract Results are given of compression tests made on 56 Dural-Celluboard Sandwich Panels with Birch Spruce or Whitewood centres. These are compared with results from similar tests on Dural-Balsa sandwich and all-metal panels, and it is seen that over the range of sizes and weights considered Dural-Celluboard can be equally or more efficient for carrying end loads. The birch Celluboard was more efficient than the spruce or whitewood and the thicker sandwiches, and those with thicker skins were more efficient than the thinner specimens. The maximum stress reached in the skin, 48,000 lb/sq in., was equal to the 0.1 per cent tensile proof stress of the material. The birch filling had also reached its maximum compression stress, 8,000 lb/sq in. The design had therefore exploited these materials to their fullest extent. en_US
dc.relation.ispartofseries Aeronautical Research Council Reports & Memoranda en_US
dc.title Compression tests on dural-celluboard sandwich panels en_US


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