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Title
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Effect Of Temperature On The Creep Of Polycrystalline Aluminum By The Cross-Sslip Mechanism
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Description
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The apparent activation energy for creep of polycrystalline aluminum was determined over the range of 273° to 350°K by the effect of small abrupt changes in temperature on the creep rate. A constant activation energy of 27,400 ± 1000 cal/mole was obtained over strains of 0.003 to 0.23, stresses ranging from 2250 to 6000 p. s. i. and strain rates varying from 0.1145 x 10-5 to 29.5 x 10-5 per minute. Metallographic studies and comparison with theory suggested that creep in this range is controlled by the rate of cross-slip of dislocations.Both X-ray diffraction analyses and room temperature tensile stress-strain data following precreep revealed that the substructure produced in this range by creep under a given stress depended only on the total creep strain being independent of the actual test temperature. As a result it was deduced that the total strain ε during creep under a given stress should be a function of temperature compensated time Θ = te-Q/RT where t is the duration of the test, Q the apparent activation energy, R the gas constant and T the absolute temperature. A number of creep tests conducted at two different temperatures verified the validity of this conclusion.
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Date
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1960
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Index Abstract
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Contrails and DTIC
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Photo Quality
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Incomplete
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Report Number
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WADD TR 60-53
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Creator
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Jaffe, N.
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Dorn, J. E.
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Corporate Author
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University Of California
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Laboratory
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Materials Central
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Extent
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21
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PB Number
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PB171360
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Identifier
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ADA328524
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ADA328524
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Access Rights
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OTS
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Distribution Classification
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1
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Contract
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AF 33(616)-3860
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DoD Project
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7360
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DoD Task
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73604
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DTIC Record Exists
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Yes
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Distribution Change Authority Correspondence
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None
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Report Availability
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Full text available
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Date Issued
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1960-06
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Abstract
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The apparent activation energy for creep of polycrystalline aluminum was determined over the range of 273° to 350°K by the effect of small abrupt changes in temperature on the creep rate. A constant activation energy of 27,400 ± 1000 cal/mole was obtained over strains of 0.003 to 0.23, stresses ranging from 2250 to 6000 p. s. i. and strain rates varying from 0.1145 x 10-5 to 29.5 x 10-5 per minute. Metallographic studies and comparison with theory suggested that creep in this range is controlled by the rate of cross-slip of dislocations.Both X-ray diffraction analyses and room temperature tensile stress-strain data following precreep revealed that the substructure produced in this range by creep under a given stress depended only on the total creep strain being independent of the actual test temperature. As a result it was deduced that the total strain ε during creep under a given stress should be a function of temperature compensated time Θ = te-Q/RT where t is the duration of the test, Q the apparent activation energy, R the gas constant and T the absolute temperature. A number of creep tests conducted at two different temperatures verified the validity of this conclusion.
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Provenance
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IIT
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Type
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report
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Format
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1 online resource (iv, 17 pages) : ill.
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Subject
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Aluminum
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Creep Tests
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Polycrystalline
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Activation Energy
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Publisher
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Wright-Patterson Air Force Base, OH : Wright Air Development Division, Air Research and Development Command, United States Air Force
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Distribution Conflict
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No