Research at North American Aviation in connection with design of Mach 3 fighter to find means to shield and insulate caps of wing support frames and wing carry-through members enclosing 2 J-93 engines; tensile properties at temperature of best high strength materials which include H-11 steels and nickel-cobalt alloys; problems involved of designing major load carrying portion of aircraft to ultra high temperatures; limited forms in which these metals can be produced; examples. (see also SAE -- J v 69 n 12 Dec 1961 p 64-5)
Reacting flight loads at forging temperatures
SAE -- Paper
SAE Meeting ; 1961 Heat resisting
1961
4 pages
Conference paper
English
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Reacting Flight Loads at Forging Temperatures
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