Please use this identifier to cite or link to this item: http://nopr.niscpr.res.in/handle/123456789/30407
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dc.contributor.authorGoswami, T-
dc.date.accessioned2015-01-19T06:31:34Z-
dc.date.available2015-01-19T06:31:34Z-
dc.date.issued2005-10-
dc.identifier.issn0975-1017 (Online); 0971-4588 (Print)-
dc.identifier.urihttp://hdl.handle.net/123456789/30407-
dc.description367-375en_US
dc.description.abstractA transition mechanism of long crack growth from structure sensitive (Regime I) to insensitive region (Regime II) was investigated at (i) room temperature under high humidity conditions, and (ii) elevated temperatures for Ti-6AI-4V alloy and other materials. Constant amplitude tests were conducted using several stress ratios (R = 0.05, 0.1, 0.4 and 0.7) for the high humidity tests and 0.1 for room and elevated temperature tests. Conventionally forged Ti-6AI-4V alloy disks, processed to the solution treated and over-aged condition, were studied for both programs. An increase in stress ratio and temperature lowered the transitional stress intensity factor range where Regime I transitioned to Regime II. Higher stress ratios (R = 0.7) accelerated the fatigue crack growth rates many times the crack growth rates obtained at lower stress ratios (R = 0.05). However, higher temperatures (345°C) influenced the crack growth rates only marginally. The mechanisms controlling elevated temperature fatigue crack growth in Ti-6AI-4V were by the secondary crack formation, striations and some cavity features on the fracture surface. The damage was localized on the α platelets, where a type dislocations found with the Burgers vectors (a/2)<11 0> g = 1010 near (10 0). en_US
dc.language.isoen_USen_US
dc.publisherNISCAIR-CSIR, Indiaen_US
dc.relation.ispartofseriesC22C14/00en_US
dc.rights CC Attribution-Noncommercial-No Derivative Works 2.5 Indiaen_US
dc.sourceIJEMS Vol.12(5) [October 2005]en_US
dc.titleLong crack growth mechanisms in Ti-6Al-4V alloyen_US
dc.typeArticleen_US
Appears in Collections:IJEMS Vol.12(5) [October 2005]

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