1991
DOI: 10.1016/0022-3115(91)90076-j
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Strength and fatigue of dispersion-strengthened copper

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Cited by 57 publications
(15 citation statements)
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“…Yield strengths of ODS alloys are shown in Figure 2. [15][16][17][18][19][20] Most of these data were obtained on GlidCop AL-15 and Al-20, which have lower strengths than the Al-25 and Al-60 alloys. The room temperature yield strength varies between 300 and 600 MPa, mainly due to different amounts of cold work (31% to 80 CW) prior to testing.…”
Section: B Yield Strengthmentioning
confidence: 99%
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“…Yield strengths of ODS alloys are shown in Figure 2. [15][16][17][18][19][20] Most of these data were obtained on GlidCop AL-15 and Al-20, which have lower strengths than the Al-25 and Al-60 alloys. The room temperature yield strength varies between 300 and 600 MPa, mainly due to different amounts of cold work (31% to 80 CW) prior to testing.…”
Section: B Yield Strengthmentioning
confidence: 99%
“…[15][16][17][18][19][20] (31 -80% Cold Work) Figure 3 -Temperature effect on the yield strength of Cu-Cr-Zr alloys [5,21] Figure 4 -Steady-state thermal creep laws for copper alloys [11,14,[23][24][25][26][27][28][29][30] Figure 6 -Cyclic stress-strain curves of copper alloys at ambient temperature [36,38] Figure 7(a) -Fatigue lifetime of copper alloys, based on total strain amplitude [3,6,8,42] Cu-Cr-Zr at 216 °C (Thomas, 1993) Cu-Cr-Zr at 300 °C (Taubenlat, 1984) Cu-Cr-Zr at 300 °C (Gorynin et al, 1992) GlidCop Al15 at 400 °C (Stephens et al, 1988) GlidCop Al15 at 472 °C (Broyles et al, 1996) Applied Stress (ksi) Figure 4 -Steady-state thermal creep laws for copper alloys [11,14,[23][24][25][26][27][28][29][30] 0.001 Figure 6 -Cyclic stress-strain curves of copper alloys at ambient temperature [36,38] …”
Section: List Of Figuresmentioning
confidence: 99%
“…12. Relationship between temperature and yield stress of copper [32]. schematic diagram was given in Fig.…”
Section: Residual Stress Analysis Of Igbt Module On Copper Microchannmentioning
confidence: 99%
“…(1-3) represent are shown in Table . [17]. The Anand model parameters of SAC305 are shown in Table . In this study the material properties for the DBC copper layers were adopted from Dong and Miller, as shown in Table [18,19]. The other material properties of alumina, SAC 305 and copper are listed in Table . Besides, it was assumed that the coefficient of thermal expansion of copper layers in DBC was temperature dependent and the CTE of SAC305 and alumina was temperature independent, as shown in Fig.…”
Section: B Materials Propertiesmentioning
confidence: 99%