Problems in designing plane around given engine with minimum of deadweight and maximum of useful load, at same time fulfilling demands for strength of all structural and control parts; tables give data on weights of items of all structural parts on which designer has direct influence; and their percentage of weight empty for Fokker Super-Universal, F-10-A, and F-32.
The airplane weight complex
Aviation
Aviation ; 29 , n 4
1930
6 pages
4 Figs.
Article (Journal)
English
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