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Journal Articles
Alloy Digest (1959) 8 (7): Al-80.
Published: 01 July 1959
... ALUMINUM 357 is a highly purity aluminum casting alloy which develops high tensile and yield strengths with good ductility after heat treatment. This datasheet provides information on composition, hardness, and tensile properties. It also includes information on corrosion resistance as well...
Abstract
View articletitled, <span class="search-highlight">ALUMINUM</span> <span class="search-highlight">357</span>: High Strength <span class="search-highlight">Aluminum</span> Alloy
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for article titled, <span class="search-highlight">ALUMINUM</span> <span class="search-highlight">357</span>: High Strength <span class="search-highlight">Aluminum</span> Alloy
ALUMINUM 357 is a highly purity aluminum casting alloy which develops high tensile and yield strengths with good ductility after heat treatment. This datasheet provides information on composition, hardness, and tensile properties. It also includes information on corrosion resistance as well as casting, heat treating, machining, and joining. Filing Code: Al-80. Producer or source: Kaiser Aluminum & Chemical Corporation.
Journal Articles
Alloy Digest (1999) 48 (1): Al-357.
Published: 01 January 1999
..., hardness, tensile properties, and shear strength as well as fatigue. It also includes information on corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: AL-357. Producer or source: Tennalum, A Division of Kaiser Aluminum. Producer or Source...
Abstract
View articletitled, KAISER <span class="search-highlight">ALUMINUM</span> ALLOY 2024: Heat Treatable Wrought <span class="search-highlight">Aluminum</span> Alloy
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for article titled, KAISER <span class="search-highlight">ALUMINUM</span> ALLOY 2024: Heat Treatable Wrought <span class="search-highlight">Aluminum</span> Alloy
Kaiser Aluminum Alloy 2024 has good machinability and good mechanical properties. The alloy is typically used in aircraft structures, rivets, connectors, hydraulic valve bodies, and miscellaneous structural applications. This datasheet provides information on composition, physical properties, hardness, tensile properties, and shear strength as well as fatigue. It also includes information on corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: AL-357. Producer or source: Tennalum, A Division of Kaiser Aluminum.
Journal Articles
Alloy Digest (1967) 16 (2): Al-163.
Published: 01 February 1967
...: After solution treating, reheat at 3400F for 3-5 hours, air cool. (Note: Water remperarure from 150-2120F can be employ- ed. Boiling water is recommended since ic minimizes quenching stresses and distortion.) Machinability: Aluminum A-357 has a high machinability rating. Both high-speed steel...
Abstract
View articletitled, <span class="search-highlight">ALUMINUM</span> A357: Sand and Permanent Mold Casting Alloy
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for article titled, <span class="search-highlight">ALUMINUM</span> A357: Sand and Permanent Mold Casting Alloy
Aluminum A357 is a high strength, pressure tight sand and permanent mold aluminum casting alloy. It is age-hardenable. It is recommended for cast gear cases, cylinder heads, transmission cases and strong structural castings. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and shear strength as well as fatigue. It also includes information on high temperature performance and corrosion resistance as well as casting, heat treating, machining, and joining. Filing Code: Al-163. Producer or source: Aluminum Company of America.
Journal Articles
Alloy Digest (1988) 37 (7): Ni-357.
Published: 01 July 1988
... Silicon 0.1 Chromium 20.5 Nickel 61 Molybdenum 8.5 Columbium 3.3 Titanium 1.3 Aluminum 0.2 Iron Remainder Tabie 1 - COMPARATIVE ROOM-TEMPERATURE TENSILE PROPERTIES* Alloy Treatment CUSTOM AGE 1800-1900°F 625 PLUS, 1-4h, WQ + 4 diam. 135&1375OF bar 8h, FC to 1 15(F1200°F hold 8h, AC 625 Cold Rolled 718...
Abstract
View articletitled, CUSTOM AGE 625 PLUS ALLOY: Precipitation Hardenable Nickel-Base Alloy
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for article titled, CUSTOM AGE 625 PLUS ALLOY: Precipitation Hardenable Nickel-Base Alloy
CUSTOM AGE 625 PLUS Alloy offers exceptional resistance to pitting, crevice, attack, general corrosion and to stress-corrosion cracking in the precipitation-hardened condition. This datasheet provides information on composition and tensile properties as well as fracture toughness. It also includes information on corrosion resistance as well as forming, heat treating, and machining. Filing Code: Ni-357. Producer or source: Carpenter Technology Corporation.
Journal Articles
Alloy Digest (2023) 72 (1): Al-493.
Published: 01 January 2023
... values. (a) Average of all tempers. Source: Aluminum 5083 (UNS A95083), Austral Wright Metals, and 5083, Properties and Selection of Aluminum Alloys, Volume 2B, ASM Handbook, ASM International, 2019, p 356 357 Mechanical Properties Austral Wright 5083 is not hardenable by heat treatment. However, it can...
Abstract
View articletitled, AUSTRAL WRIGHT 5083: Al-4.5Mg-0.7Mn-0.15Cr Alloy
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for article titled, AUSTRAL WRIGHT 5083: Al-4.5Mg-0.7Mn-0.15Cr Alloy
Austral Wright 5083 is a wrought, non-heat-treatable, aluminum-magnesium-manganese-chromium alloy (5xxx series). It has the highest strength of the non-heat-treatable alloys but is not recommended for use at temperatures in excess of 65 °C (150 °F). It is among the most widely used aluminum alloys for marine applications. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on corrosion resistance as well as forming, heat treating, and joining. Filing Code: Al-493. Producer or source: Austral Wright Metals.
Journal Articles
Alloy Digest (1995) 44 (6): Cu-601.
Published: 01 June 1995
...: Nickel 14.5 Manganese 4.5 Copper Bal. *Strengthened with additions of aluminum and iron, which may be refined by small amounts of chromium. PROPERTIES Tabfe 1 - MINIMUM MECHANICAL PROPERTIES FOR BAR AND FORGINGS (R.T.) Ban Bars Forgings, and below 15 mm of diameter bars of diameter dimn6ter 15-125 mm...
Abstract
View articletitled, HIDURON ALLOY 191: High Strength Precipitation Hardened Copper Nickel
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for article titled, HIDURON ALLOY 191: High Strength Precipitation Hardened Copper Nickel
HIDURON alloy 191 was developed for marine applications where both a combination of strength and good corrosion/ impingement resistance is needed. It finds applications in shafts, fasteners and valve stems. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: CU-601. Producer or source: Langley Alloys Ltd.
Journal Articles
Alloy Digest (2011) 60 (5): SA-625.
Published: 01 May 2011
... 0.22 0.54 Chromium < 0.30 < 0.35 Niobium 0.15 0.45 0.005 0.055 Aluminum tot >0.015 >0.010 Physical Properties: Density (approximate), kg/cm3 (lb/in.3) 7750 (0.280) Mechanical Properties: Mechanical properties at ambient temperature are given in Table 1 while elevated proof stress is given...
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View articletitled, DIWA 373: Weldable Steel for Higher Temperature Service
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for article titled, DIWA 373: Weldable Steel for Higher Temperature Service
DIWA 373 can be used for temperatures up to 500 C and is suitable for use in boilers and piping systems. It is available in thicknesses up to 250 mm (9.84 in.). Up to a thickness of 180 millimeter, it is supplied in normalized and tempered state, and above this thickness, water-quenched and tempered. DIWA 373 is based on the standardized 15NiCuMoNb5 grade. (Material No. 1.6368) EN 10028, Part 2. This datasheet provides information on composition, physical properties, and tensile properties as well as fracture toughness and creep. It also includes information on high temperature performance as well as forming, heat treating, and joining. Filing Code: SA-625. Producer or source: Dillinger Hütte GTS.
Journal Articles
Alloy Digest (2022) 71 (2): CS-216.
Published: 01 February 2022
..., aluminum bronze, copper, zinc, lead-tin solders, lithium, cadmium and indium. The degree of embrittlement is greater for steels that have been heat treated to produce higher strength. Source: Ref 22 Corrosion in Fresh Water. The average corrosion rate of nonalloy steels in stagnant air-saturated soft...
Abstract
View articletitled, SAE 1039, SAE 1040, CEN C40, ISO C40 STEEL DATA SURVEY: Wrought Medium-Carbon Non-Alloy Steels
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for article titled, SAE 1039, SAE 1040, CEN C40, ISO C40 STEEL DATA SURVEY: Wrought Medium-Carbon Non-Alloy Steels
1039, 1040, C40, C40E, and C40R are wrought medium-carbon non-alloy steels that are used in the normalized, cold worked, or quenched and tempered condition. 1039, 1040, C40E, and C40R may also be flame or induction hardened. These steels are widely used for moderately stressed parts that require higher strength levels than can be achieved by the lower carbon grades, and where the expense of an alloy steel is not justified. Owing to their low hardenability their use in the quench and tempered condition is not recommended for large sizes, as the improvement in mechanical properties over the normalized condition is insufficient to justify the additional cost of heat treatment. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joinability. Filing Code: CS-216. Producer or source: Data Survey.
Journal Articles
Alloy Digest (2023) 72 (5): CS-246.
Published: 01 May 2023
... of the austenite grains is due to the dissolution of small aluminum nitride precipitates that were pinning the grain boundaries (which are much too small to be seen in the light microscope and must be examined in the transmission electron microscope). Once the particles dissolved upon heating, the grain boundaries...
Abstract
View articletitled, SAE 1039, SAE 1040, CEN C40, ISO C40: Wrought Medium-Carbon Non-Alloy Steels
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for article titled, SAE 1039, SAE 1040, CEN C40, ISO C40: Wrought Medium-Carbon Non-Alloy Steels
1039, 1040, C40, C40E, and C40R are wrought medium-carbon (carbon = 0.37–0.44%) non-alloy steels that are used in the normalized, cold worked, or quenched and tempered condition. 1039, 1040, C40E, and C40R may also be flame or induction hardened, nitrided, or nitrocarburized. These steels are widely used for moderately and highly stressed parts that require higher strength levels than can be achieved by the lower carbon grades, and where the expense of an alloy steel is not justified. Owing to their low hardenability their use in the quench and tempered condition is not recommended for large sizes, as the improvement in mechanical properties over the normalized condition is insufficient to justify the additional cost of heat treatment. This datasheet provides information on composition, physical properties, hardness, and tensile properties. It also includes information on forming and heat treating. Filing Code: CS-246. Producer or source: Heat Treater's Guide.