Study of tensile properties to evaluate strength potential available in titanium alloys, precipitation hardening, and cold worked metastable austenitic stainless steels, and super alloys; unstable crack propagation resistance under static loading; stability under long time load and temperature; nonsteady load and temperature; it is possible to define alloys and assess important variables in design of Mach 3 aircraft. (see also abstract in SAE -- J v 69 n 7, 8 July 1961 p 32-6, Aug p 84-7)
Considerations in selection of wing and fuselage sheet materials for trisonic transports
SAE -- Paper
SAE Meeting ; 1961
1961
19 pages
Conference paper
English
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Considerations in Selection of Wing and Fuselage Sheet Materials for Trisonic Transports
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