Metallic materials and elements for aerospace vehicle by United States. Dept. of Defense

By United States. Dept. of Defense

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E, 103 ksi . . . . . . Ec, 103 ksi . . . . . . G, 103 ksi . . . . . . µ ................. 3 . . . . . . C, Btu/(lb)(·F) . . . . K, Btu/[(hr)(ft2 )(·F)/ft] . /·F . . . . AMS 5046 and MIL-S-7952 Sheet, strip, and plate Annealed ... S AMS 5075, AMS 5077 and AMS-T-5066a Tubing Normalized ... S 55 55 ... 55 55 ... 55 55 55 36 36 ... 36 36 ... 36 36 36 36 36 ... 35 36 36 ... 35 36 36 36 35 ... 90 ... 90 ... 90 ... ... ... ... c c c ... 32 ... 0 a Noncurrent specification.

Fty, ksi: L ................ LT . . . . . . . . ST . . . . . . . . Fcy, ksi: L ................ LT . . . . . . . . ST . . . . . . . . Fsu , ksi . . . . . . . 5) . . . . . 0) . . . . . 5) . . . . . 0) . . . . . e, percent: L ................ LT . . . . . . . . E, 103 ksi . . . . . . Ec, 103 ksi . . . . . . G, 103 ksi . . . . . . µ ................. 3 . . . . . . C, Btu/(lb)(·F) . . . . K, Btu/[(hr)(ft2 )(·F)/ft] .

Values of Room Temperature Plane-Strain Fracture Toughness of Steel Alloys  Alloy Heat Treat Condition Product Form Orientationb Yield Strength Range, ksi Product Thickness Range, inches Number of Sources Sample Size Specimen Thickness Range, inches Max. Avg. Min. Coefficient of Variation KIC, ksi in. 5 a These values are for information only. 3 for definition of symbols. 2 Physical Properties — The physical properties (, C, K, and ) of steels may be considered to apply to all forms and heat treatments unless otherwise indicated.

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