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t.a
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Published: 01 December 2008
Fig. 9.8 The T-T-T diagram for γ → α transformation of steel (the isothermal transformation diagram). The transformation of pure iron is interface control. The transformation of Fe-C alloys is diffusion control of C atoms.
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Published: 01 September 2022
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Published: 30 November 2013
Fig. 7 Effect of elevated temperatures T 1 and T 2 on tensile and compressive properties of a typical metal
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in Life Assessment of Steam-Turbine Components
> Damage Mechanisms and Life Assessment of High-Temperature Components
Published: 01 December 1989
Fig. 6.24. Resistivity technique for estimating life fraction, t/t r , expended in creep ( Ref 46 ). (a) Resistivity ratio as a function of exposure condition. (b) Decrease in resistivity ratio with expended creep life.
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in Life-Assessment Techniques for Combustion Turbines
> Damage Mechanisms and Life Assessment of High-Temperature Components
Published: 01 December 1989
Fig. 9.41. Gamma-prime particle size as a function of t 1/3 (t is time of thermal exposure) for superalloys (based on Ref 7 , 8 , 64 , and 69 ).
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Published: 01 December 2003
Fig. 1 Log relaxation modulus, E ( t ), as a function of log time, t (or temperature), for a glassy thermoplastic material. 1, glassy plateau; 2, transition region; 3, rubbery plateau; 4, flow region. T g , glass transition temperature
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Published: 01 August 2012
Fig. 5.14 Effect of strain rate on flow stress ( t 0 = 1 mm; T = 200 °C, or 390 °F). Source: Ref 5.6
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in Plastic Deformation: Flow Stress, Anisotropy, and Formability
> Sheet Metal Forming: Fundamentals
Published: 01 August 2012
Fig. 4.15 Schematic of hydraulic bulge test ( t 0 = original sheet thickness, t = sheet thickness at the apex, h d = bulge height, P = hydraulic pressure, r f = die fillet radius, r c = die cavity radius)
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in Dealing with Friction in Design Engineering
> Tribomaterials: Properties and Selection for Friction, Wear, and Erosion Applications
Published: 30 April 2021
Fig. 3.8 Schematic of commonly used friction tests; N, load; F, friction force; T, tension
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Published: 01 June 1983
Figure 2.14 Plot of C / T vs. T 2 to yield β (slope) and γ (intercept) for the specific heat formula, Eq. 2.64 . Experimental data are shown for copper ( Franck, Manchester, and Martin, 1961 ), aluminum ( Kok and Keesom, 1937 ), and Nal ( Clayton and Marshall, 1960 )
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Published: 01 June 1983
Figure 2.16 Plot of C / T vs. T 2 for stainless steel AISI 3I0S ( Jelinek and Collings, 1975a ). The rapid increase in C / T at low temperatures is a manifestation of the constant term in the specific heat formula ( Eq. 2.69 ).
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Published: 30 November 2013
Fig. 1 Elastic stress distribution: pure tension. T, tension. C, compression. (a) No stress concentration. (b) Surface stress concentrations. (c) Transverse hole stress concentration
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Published: 30 November 2013
Fig. 3 Elastic stress distribution: pure compression. T, tension. C, compression. (a) No stress concentration. (b) Surface stress concentrations. (c) Transverse hole stress concentration
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Published: 30 November 2013
Fig. 4 Elastic stress distribution: pure bending. T, tension. C, compression. (a) No stress concentration. (b) Transverse surface stress concentrations
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Published: 30 November 2013