ASD Technical Report, Numéro 62Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1963 |
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2014-T6 Aluminum Alloy 301 Stainless Steel 4-inch-wide 78 Long 81 Aluminum Alloy Aeronautical Systems Division Aluminum Alloy 0.063 Aluminum Company base metal cold-rolled Company of America complex welded joints Crack Extension Force crack propagation specimens crack propagation tests cross-tensile CRYOGENIC ENVIRONMENT cryogenic temperatures cryostat Elastic Modulus elongation embrittlement Etchant evaluation Failed statically failure 1 Long Fatigue Crack Growth fatigue specimens fatigue tests Figure filler metal fracture toughness GC values grain direction Heat heat-affected zone high strength in-lb/in² increase individual resistance spot load rate Longitudinal Specimens Mechanical Properties notch length notched tensile NUMBER OF CYCLES percent PHYSICAL AND MECHANICAL PRESSURE VESSEL Rene René 41 Alloy resistance spot welds room temperature sheet alloys sheet materials specimen width Stainless Steel Longitudinal static joint static tests stress stress concentration Temp tensile data tensile tests tensile-shear Tension test specimens testing temperatures tests were performed titanium Ultimate Lb UNCLASSIFIED WTSL yield strengths