Abstract
The following method of calculating the stresses in the spars of an aeroplane wing is essentially a simplification in form of the method given in the paper “Some Contributions to the Theory of Engineering Structures, with special reference to the Problem of the Aeroplane,” by Messrs. H. Booth and H. Bolas, issued by the Air Department of the Admiralty in April, 1915.
Publisher
Cambridge University Press (CUP)
Cited by
5 articles.
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