Problem at subsonic speeds; trend towards use of large single piece aircraft components; use of alloy steel; advantages of titanium alloys at temperature of 200 F; above 700 F, stainless steel and cobalt base alloys seem to be most promising; usable flight spectra of various materials discussed are shown graphically.
Selection of aircraft construction materials
Soc Automotive Engrs -- Paper
Society of Automotive Engineers -- Meeting ; 1954 Selection
1954
5 pages
Conference paper
English
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SELECTION OF AIRCRAFT CONSTRUCTION MATERIALS
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