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Strain history paths for (a) time-hardening and (b) strain-hardening approa...
Available to PurchasePublished: 01 November 2010
Fig. 8 Strain history paths for (a) time-hardening and (b) strain-hardening approaches for variable stress histories
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Published: 01 January 2006
Fig. 7 Dependence of the strain-hardening exponent, n , on strain rate for steels. Adapted from Ref 7
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Published: 01 January 2005
Fig. 7 Dependence of the strain-hardening exponent, n , on strain rate for steels. Adapted from Ref 7
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Published: 01 January 2005
Fig. 6 Log-log plot of true stress-true strain curve. n is the strain-hardening exponent; K is the strength coefficient
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Published: 01 January 2005
Fig. 7 Log-log plot of true-stress/true-strain curve. n is the strain-hardening exponent; K is the strength coefficient.
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Comparison of the engineering stress-strain curves for non-strain-hardening...
Available to PurchasePublished: 01 January 2005
Fig. 25 Comparison of the engineering stress-strain curves for non-strain-hardening samples without or with a 1 or 2% taper predicted using the direct-equilibrium approach. Source: Ref 29
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Published: 01 January 2000
Fig. 8 Log-log plot of true stress-true strain curve n is the strain-hardening exponent; K is the strength coefficient.
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True stress vs. true strain (solid lines) and strain-hardening rate (dashed...
Available to PurchasePublished: 30 June 2023
Fig. 5 True stress vs. true strain (solid lines) and strain-hardening rate (dashed lines) curves of the studied laser powder-bed fusion 316L strained at (a) higher (0.008 s −1 ) and (b) lower (0.0005 s −1 ) strain rates. VED, volumetric energy density. Source: Ref 12
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Effect of heat treatment and strain hardening on the ductility and ductile-...
Available to PurchasePublished: 01 January 2006
Fig. 1 Effect of heat treatment and strain hardening on the ductility and ductile-to-brittle transition temperature range of unalloyed molybdenum sheet as determined in tensile tests. The ductile-to-brittle transition occurs in the temperature range in the steep portion of the ductility curves.
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Published: 01 January 2006
Fig. 8 Decrease of the strain-hardening exponent, n , of pure aluminum with temperature. Adapted from Ref 8
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Internal strength is the sum of the net increments from strain hardening an...
Available to PurchasePublished: 01 January 2006
Fig. 15 Internal strength is the sum of the net increments from strain hardening and dynamic recovery components. The rate of the former is obtained from the basic hardening curve (same for the same level of g ) and decreases with increasing g , while that of the latter increases. The basic
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Influence of speed, tool geometry, and prior strain hardening on the specif...
Available to PurchasePublished: 01 January 1989
Fig. 7 Influence of speed, tool geometry, and prior strain hardening on the specific energy of brass
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Change in residual strain hardening during isothermal recovery for zone-mel...
Available to PurchasePublished: 01 January 2005
Fig. 7 Change in residual strain hardening during isothermal recovery for zone-melted iron deformed 5% in tension at 0 °C (32 °F). The fraction of residual strain hardening, 1− R =(σ−σ 0 )/(σ m −σ 0 ), where R is the fraction of recovery, σ 0 the flow stress of the fully annealed material
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Published: 01 January 2005
Fig. 8 Decrease of the strain-hardening exponent, n , of pure aluminum with temperature. Adapted from Ref 8
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Image
Internal strength is the sum of the net increments from strain hardening an...
Available to PurchasePublished: 01 January 2005
Fig. 15 Internal strength is the sum of the net increments from strain hardening and dynamic recovery components. The rate of the former is obtained from the basic hardening curve (same for the same level of g ) and decreases with increasing g , while that of the latter increases. The basic
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Change in residual strain hardening during isothermal recovery for zone-mel...
Available to PurchasePublished: 01 December 2004
Fig. 7 Change in residual strain hardening during isothermal recovery for zone-melted iron deformed 5% in tension at 0 °C (32 °F). The fraction of residual strain hardening, 1 − R = (σ − σ 0 ) ÷ (σ m − σ 0 ), where R is the fraction of recovery, σ 0 the flow stress of the fully annealed
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Strain-hardening curves for aluminum (1100), Al-Mn (3003) alloys, and Al-Mg...
Available to PurchasePublished: 01 December 1998
Fig. 5 Strain-hardening curves for aluminum (1100), Al-Mn (3003) alloys, and Al-Mg (5050 and 5052) alloys
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Threshold load for seizure versus strain-hardening exponent for various ste...
Available to PurchasePublished: 31 December 2017
Fig. 17 Threshold load for seizure versus strain-hardening exponent for various steels. Source: Ref 12
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Effects of environment on the yield stress and strain-hardening rate on var...
Available to PurchasePublished: 01 January 2003
Fig. 1 Effects of environment on the yield stress and strain-hardening rate on various iron-aluminum alloys tested in air and mercury-indium solutions
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Strain-hardening curves for aluminum (1100) and for aluminum-manganese (300...
Available to PurchasePublished: 30 November 2018
Fig. 5 Strain-hardening curves for aluminum (1100) and for aluminum-manganese (3003) and aluminum-magnesium (5050 and 5052) alloys
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