THE paper by Dr J. H. ARGYRIS which we publish in this issue is of unusual interest and importance. In conjunction with Mr P. C. DUNNE the author has been responsible for great development in the science of stressing of aircraft structures. Their theories were expounded in detail in the Journal of the Royal Aeronautical Society in 1947 and 1949 and they were responsible for much of the work on the early stressed‐skin data sheets issued by the Society.
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