Analysis of factors controlling structural efficiency with particular regard to cantilever design of Fokker plane; aspect ratio, design load, wing area and maximum wing chord; selection of basic structure and best suited material; increasing structural efficiency to save 4 1/2 per cent of weight of empty airplane will give 13 1/2 per cent increase in payload without increasing gross weight.
Weight savings by structural efficiency
Soc. Automotive Engrs. -- Jl
Society of Automotive Engineers -- Journal ; 27 , n 4
1930
Article (Journal)
English
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