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 -- Paper 420D for meeting Oct 9-13 1961 4 p)
Reacting flight loads at forging temperatures
SAE -- J
Society of Automotive Engineers -- Journal ; 69 , n 12
1961
2 pages
Article (Journal)
English
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Reacting Flight Loads at Forging Temperatures
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