Formulas giving rational criteria for design of airplane members and for selection of most suitable materials, taking due account of physical properties of aircraft materials and of resistance that results from proper use of each; tables of relative strength values show which materials are best for various parts and how much weight it is wise to add for given reduction in parasite resistance or for given increase in output of power plant; properties of various materials are studied separately with relation to their functions, and indexes are given classifying them in order of their merit for tension and compression, and for beams and columns.
Selection of materials for aircraft structures
Soc. Automotive Engrs. -- Jl.
Society of Automotive Engineers -- Journal ; 21 , n 5
1927
3 pages
Article (Journal)
English
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Selection of Materials for Aircraft Structures
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