Behavior of Three Metallic Alloys Under Combined Axial-shear Stress at 650 C Final Report ... Nasa PDF Download
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Author: United States. National Aeronautics and Space Administration
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Category :
Languages : en
Pages :
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Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 168
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Category : Government publications
Languages : en
Pages : 1102
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Author: PJ. Bonacuse
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Category : Axial-torsional loading
Languages : en
Pages : 26
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The cyclic, high-temperature deformation behavior of a wrought cobalt-base superalloy, Haynes 188, is investigated under combined axial and torsional loads. This is accomplished through the examination of hysteresis loops generated from a biaxial fatigue test program. A high-temperature axial, torsional, and combined axial-torsional fatigue database has been generated on Haynes 188 at 760°C. Cyclic loading tests have been conducted on uniform gage section tubular specimens in a servohydraulic axial-torsional test rig. Test control and data acquisition were accomplished with a minicomputer. The fatigue behavior of Haynes 188 at 760°C under axial, torsional, and combined axial-torsional loads and the monotonic and cyclic deformation behaviors under axial and torsional loads have been previously reported. In this paper, the cyclic hardening characteristics and typical hysteresis loops in the axial stress versus axial strain, shear stress versus engineering shear strain, axial strain versus engineering shear strain, and axial stress versus shear stress spaces are presented for cyclic in-phase and out-of-phase axial-torsional tests. For in-phase tests, three different values of the proportionality constant, ? (the ratio of engineering shear strain amplitude to axial strain amplitude, ?a/?a), are examined, viz., 0.86, 1.73, and 3.46. In the out-of-phase tests, three different values of the phase angle, (between the axial and engineering shear strain waveforms), are studied, viz., 30, 60, and 90° with ? = 1.73. The cyclic hardening behaviors of all the tests conducted on Haynes 188 at 760°C are evaluated using the von Mises equivalent stress-strain and the maximum shear stress-maximum engineering shear strain (Tresca) curves. Comparisons are also made between the hardening behaviors of cyclic axial, torsional, and combined in-phase (? = 1.73 and = 0°) and out-of-phase (? = 1.73 and = 90°) axial-torsional fatigue tests. These comparisons are accomplished through simple Ramberg-Osgood type stress-strain functions for cyclic, axial stress-strain and shear stress-engineering shear strain curves.
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Category : Aeronautics
Languages : en
Pages : 500
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Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 230
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Author: Richard T. Barrett
Publisher:
ISBN: 9781304069542
Category :
Languages : en
Pages :
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ISBN:
Category : Government reports announcements & index
Languages : en
Pages : 882
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Author:
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Category : Power resources
Languages : en
Pages : 1162
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Author:
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Category : Metallurgy
Languages : en
Pages : 628
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