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Books on the topic 'Creep of aluminum'

Author: Grafiati
Published: 4 June 2021
Last updated: 8 February 2022

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1

de, Villiers H. L., ed. The physics of creep: Creep and creep-resistant alloys. London: Taylor & Francis, 1995.

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2

Taylor, David Wayne. The Lithium concentration dependence of creep in binary Aluminum-Lithium alloys. Monterey, Calif: Naval Postgraduate School, 1989.

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3

Ansari, Iqbal. Irradiation-Induced Creep and Microstructural Development in Precipitation-Hardened Nickel-Aluminum Alloys. Julich, W. Ger: Zentralbibliothek der Kernforschungsanlage, 1985.

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4

Whittenberger, J. Daniel. Elevated temperature creep properties of NiAl cryomilled with and without Y₂O₃. [Washington, D.C: National Aeronautics and Space Administration, 1995.

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5

Durman, Mehmet. The creep behaviour of pressure diecast zinc-aluminium based alloys. Birmingham: Aston University. Department of Production and Mechanical Engineering, 1989.

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6

Ortiz, Ramiro O. Biaxial creep behavior of an aluminum alloy with oriented grain structure. 1987.

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7

C, Goldsby Jon, and United States. National Aeronautics and Space Administration., eds. Tensile creep behavior of polycrystalline alumina fibers. [Washington, DC]: National Aeronautics and Space Administration, 1993.

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8

C, Goldsby J., and United States. National Aeronautics and Space Administration., eds. Tensile creep behavior of polycrystalline alumina fibers. [Washington, DC]: National Aeronautics and Space Administration, 1993.

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9

Kaufman, J. Gilbert, and Elwin L. Rooy. Aluminum Alloy Castings. ASM International, 2004. http://dx.doi.org/10.31399/asm.tb.aacppa.9781627083355.

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Abstract:
Aluminum Alloy Castings: Properties, Processes and Applications is a practical guide to the process, structure, property relationships associated with aluminum alloy castings and casting processes. It covers a wide range of casting methods, including variations of sand casting, permanent mold casting, and pressure die casting, showing how key process variables affect the microstructure, properties, and performance of cast aluminum parts. Other chapters provide similar information on the effects of alloying and heat treating and the influence and control of porosity and inclusions. A significant portion of the book contains curated collections of property and performance data, including many previously unpublished aging response curves, growth curves, and fatigue curves; tensile properties at high and low temperatures and at room temperature after high-temperature exposure; the results of creep rupture tests conducted at temperatures from 212 to 600 °F (100 to 315 °C); and stress-strain curves obtained from casting alloys in various tempers under tensile or compressive loads. The book also discusses the factors that contribute to corrosion and fracture resistance and includes test specimen drawings as well as a glossary of terms. For information on the print version, ISBN 978-0-87170-803-8, follow this link.
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10

Kaufman, J. Gilbert. Properties of Aluminum Alloys: Tensile, Creep, and Fatigue Data at High and Low Temperatures (#09813G). ASM International, 2000.

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11

McMahon, Michael E. The variation of subgrain misorientation in aluminum with large steady-state creep strain. 1986.

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12

J, Cawley, Greenwood G. W, Strang A, and Institute of Materials (London, England)., eds. Microstructural stability of creep resistant alloys for high temperature plant applications. London: IOM Communications, 1998.

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13

Wetter, Timothy Scott. The variation of the dislocation density in aluminum deformed to large steady-state creep strains. 1986.

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14

Mieszczanski, Paul P. The variation in the subgrain size in aluminum deformed to large steady-state creep strains. 1985.

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15

(Editor), Andrew Strang, J. Cawley (Editor), and G. W. Greenwood (Editor), eds. Microstructural Stability of Creep Resistant Alloys for High Temperature Plant Applications (Microstructure of High Temperature Materials). Ashgate Publishing, 1998.

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16

Characterization of metal matrix composites. [Washington, DC]: National Aeronautics and Space Administration, 1994.

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17

R, Johnson D., and United States. National Aeronautics and Space Administration., eds. NiAl-based polyphase in situ composites in the NiAl-Ta-X (X = Cr, Mo, or V) systems. [Washington, D.C: National Aeronautics and Space Administration, 1995.

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18

Yun, H. M. Tensile creep behavior of polycrystalline alumina fibers. 1993.

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19

C, Goldsby Jon, DiCarlo James A, and United States. National Aeronautics and Space Administration., eds. Stress-rupture behavior of small diameter polycrystalline alumina fibers. [Washington, DC]: National Aeronautics and Space Administration, 1993.

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20

C, Goldsby Jon, DiCarlo James A, and United States. National Aeronautics and Space Administration., eds. Stress-rupture behavior of small diameter polycrystalline alumina fibers. [Washington, DC]: National Aeronautics and Space Administration, 1993.

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21

C, Goldsby J., DiCarlo James A, and United States. National Aeronautics and Space Administration., eds. Stress-rupture behavior of small diameter polycrystalline alumina fibers. [Washington, DC]: National Aeronautics and Space Administration, 1993.

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22

C, Goldsby Jon, DiCarlo James A, and United States. National Aeronautics and Space Administration., eds. Stress-rupture behavior of small diameter polycrystalline alumina fibers. [Washington, DC]: National Aeronautics and Space Administration, 1993.

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23

C, Goldsby J., and Lewis Research Center, eds. Annealing effects on creep and rupture of polycrystalline alumina-based fibers. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

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