1990
DOI: 10.1557/jmr.1990.0769
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Evolution of the microstructure of cobalt during diffusionless transformation cycles

Abstract: Differential scanning calorimetry and transmission electron microscopy have been used to study thermal fatigue due to diffusionless phase transformation cycling in pure cobalt. Thermal cycling through the allotropic (hep ** fee) transformation results in a temperature shift of the calorimetric peaks, which means a delay of the transformation. In addition, the transformation enthalpy, which is greater on heating than on cooling, diminishes when the number of transformation cycles increases. This is interpreted … Show more

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Cited by 12 publications
(12 citation statements)
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“…This was first reported by Adams and Altstetter 65 and confirmed by Munier et al 74 who found a difference ⌬h h Ϫ⌬h c Ӎ5 cal mol Ϫ1 . Both studies also show that when the number of transformation cycles increases ⌬h diminishes and the hysteresis width increases.…”
Section: E Irreversibility Of the Latent Heat And The Intermediate 6supporting
confidence: 64%
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“…This was first reported by Adams and Altstetter 65 and confirmed by Munier et al 74 who found a difference ⌬h h Ϫ⌬h c Ӎ5 cal mol Ϫ1 . Both studies also show that when the number of transformation cycles increases ⌬h diminishes and the hysteresis width increases.…”
Section: E Irreversibility Of the Latent Heat And The Intermediate 6supporting
confidence: 64%
“…Both studies also show that when the number of transformation cycles increases ⌬h diminishes and the hysteresis width increases. 65,74 A similar interpretation of this ''irreversible'' behavior is proposed by the two groups of searchers: Cycling through the transformation induces defects in the two close packed structures and the difference found for ⌬h h Ϫ⌬h c is due to the amount of energy needed for their formation. The fact that ⌬h h is larger that ⌬h c is consistent with the property assumed in our description, that the fcc phase is more ordered than the hcp phase: More energy will be required to create defects in the fcc phase when heating from hcp, than in the hcp phase, on cooling from fcc.…”
Section: E Irreversibility Of the Latent Heat And The Intermediate 6mentioning
confidence: 59%
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“…4, T 0 = 690±7 K (at 1 atm), covers the range of most of the available literature data [2,9,11,18], based on calculations or determined experimentally, taken as average of the "austenite" and "martensite" start temperatures, measured by X-ray diffractometry, magnetometry, dilatometry or calorimetry. Values for the martensite start temperature M S range from 692 K to 661 K and for the austenite start temperature A S range from 694 K to 720 K [2,7,10] , range from 377 to 464 J mol -1 [1,2,9,11,18] and some studies indicate differences upon heating and cooling [10,15]. The diversity of these results appears to depend on the specimen shape (thin layer [6,16,17], powder [3,5,12], sheet [8,10,13,15] and rod [1,3,5,7]), the specimen size [10,15], the state of stress [7,12] and the (type of) thermal treatment [1, 3 -8, 10, 12, 15].…”
Section: Introductionmentioning
confidence: 99%