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  • 2005-2009  (2)
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  • 1
    Electronic Resource
    Electronic Resource
    s.l. ; Stafa-Zurich, Switzerland
    Advanced materials research Vol. 47-50 (June 2008), p. 515-518 
    ISSN: 1662-8985
    Source: Scientific.Net: Materials Science & Technology / Trans Tech Publications Archiv 1984-2008
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics
    Notes: The magnetic domain structures of the cubic parent phase (high-temperature phase) inferromagnetic shape memory alloys (SMAs) have been studied by electron holography. In aNi51Fe22Ga17 alloy, the magnetic flux distribution in the parent phase changes dramatically beforethe onset of martensitic transformation. In contrast, a Ni45Co5Mn36.7In13.3 alloy—a recentlydeveloped ferromagnetic SMA—does not show appreciable changes in the magnetic domainstructure upon cooling. The anomaly observed in the Ni51Fe22Ga17 alloy appears to be due tolattice distortions, which become more pronounced as the temperature approaches the martensitictransformation start temperature, Ms
    Type of Medium: Electronic Resource
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  • 2
    Electronic Resource
    Electronic Resource
    PO Box 1354, 9600 Garsington Road, Oxford OX4 2XG, UK. : Blackwell Science Ltd
    Fatigue & fracture of engineering materials & structures 28 (2005), S. 0 
    ISSN: 1460-2695
    Source: Blackwell Publishing Journal Backfiles 1879-2005
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics
    Notes: In order to investigate the crack path in materials containing a small crack under mixed mode loading, reversed torsion and combined push–pull/torsion fatigue tests were carried out on 0.47% carbon steel specimens containing an initial small crack. The initial small cracks were introduced by a preliminary push–pull fatigue test using a specimen that contained an artificial small hole of 40 μm diameter/depth. Push–pull fatigue tests followed by reversed torsion, and reversed torsion followed by push–pull were carried out. Fatigue tests of combined push–pull/torsion followed by push–pull were also carried out to examine the effect of crack geometry, such as branching and kinking, on cumulative fatigue damage. Different crack growth behaviours due to different loading modes and sequences complicatedly influenced the fatigue crack path and eventually the cumulative fatigue damage. Thus, existing fatigue damage theories cannot be applied to the cases presented in this study. A single factory roof morphology was formed on the fracture surface of the specimen having an initial semielliptical surface crack under cyclic torsion. Taking the result into consideration, torsional fatigue tests of circumferentially cracked specimens were carried out to investigate the Mode III crack growth threshold and the formation mechanism of the factory roof. It was found that the factory-roof pattern was formed by Mode I crack branching from small semielliptical cracks nucleated ahead of the circumferential crack tip. Thus, stress intensity factors at the semielliptical crack tip ahead of the circumferential crack tip were analysed to make the mechanism of crack branching from the semielliptical crack clear. The analysis shows that the Mode III stress intensity factor, KIII, at the deepest point of the semielliptical crack decreases with increase in the depth of semielliptical crack. It follows that as the shear crack growth becomes difficult at the semielliptical crack tip, crack branching starts at the major axis ends in the direction for Mode I growth, forming factory roof, due to ΔKIth 〈 ΔKIIIth.
    Type of Medium: Electronic Resource
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