Engineering Physics of High-Temperature Materials. Nirmal K. Sinha

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Engineering Physics of High-Temperature Materials - Nirmal K. Sinha

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alt="ModifyingAbove epsilon With ampersand c period dotab semicolon"/> v = ε v/t SR for the period t = 0+ to t SR. How does ε d vary with time? How does ModifyingAbove epsilon With ampersand c period dotab semicolon v vary with time, stress, temperature, and initial (constant) microstructure?

      Why not stop the test, unload the specimens completely (unlike partial unloading used in “strain‐ or stress‐transient dip tests”) during the creep test, as well as during other tests, such as constant‐strain‐rate strength tests and constant‐strain SRTs, and monitor the strain–time response for extended periods and evolution of strain trinity? This is like looking backward (hindsight) at the growth history of elastic, delayed elastic, and viscous characteristics.

      This book revolves around the concept of opening up the door for hindsight and using the opportunity it offers for developing both experimental and theoretical approaches. This is a recurring theme of various chapters. Experimental procedures were developed to examine not only total deformation, but also the three strain components: elastic, recoverable delayed elastic, and permanent viscous strain. Most importantly, theoretical developments can also be judged not only by how well they predict the total deformation under specific external conditions, but also how well they predict the strain components.

      It is well known that viscous flow (dislocation creep creep) exhibits stress‐wise highly nonlinear response, with stress exponent, n v, varying from a value of 4 for pure metals to significantly higher values for complex alloys. It is shown in Chapters 5 and 6 that delayed elastic response could exhibit nearly linear to highly nonlinear response, with stress exponent, s, varying from 1 to 4 for complex nickel‐base superalloys, so far examined experimentally. However, the ratio, n v/s, may not vary significantly for different materials examined so far. The n v/s (n v = 11.8 and s = 4.0) ratio of ≈3 for the nickel‐base superalloy IN‐738LC is similar to that of 4.3 for another nickel‐base superalloy – Waspaloy is also very close to that of 3.3 for titanium‐base alloy Ti‐6246 (n v = 4 and s = 1.2) and is exactly like that of polycrystalline ice with n v/s = 3 (n v = 3 and s = 1); however, ice is not a metal!

Schematic illustration of short-term (200 s) and longer-term (2341 s) tensile SRRTs on a single specimen of polycrystalline nickel-base superalloy Waspaloy at 1005 K (732 degrees Celsius) for 650 MPa using linear timescale.

      Source: N. K. Sinha.

      There are innumerable sets of creep curves for a wide variety of manufactured and natural materials illustrating transient and tertiary creep stages, but the recovery on full unloading is rarely reported. There are, however, examples of stress‐dip tests in which creep continues after a short recovery on partial unloading during the steady state or actually at mcr that occurs at evolved microstructure corresponding to this state. Unfortunately, stress‐dip tests do not provide useful information on transient creep at the beginning of a creep test and the characteristics of neither the delayed elastic deformation nor the viscous flow corresponding to the original, undeformed and undamaged microstructure.

      Figure 1.4 exemplifies a unique set of results for a complex nickel‐based aerospace alloy. It brings out the fact that the delayed elastic strain, ε d, recovered on full unloading well within the tertiary stage of creep, after mcr, was not negligible and not “absorbed” within the viscous component. The long‐term test (2341 s) is noticeably larger than that of the 200 s test. Hence, ε d increases with time. This raises the question as to the mechanism(s) responsible for generating delayed elasticity in polycrystalline materials that may have far‐reaching consequences, presented in Chapter 5, in developing physically based creep models.

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