Creep-Resistant Steels

Creep-Resistant Steels

Woodhead Publishing Series in Metals and Surface Engineering
2008, Pages 446-471
Creep-Resistant Steels

16 - Creep fatigue behaviour and crack growth of steels

https://doi.org/10.1533/9781845694012.2.446Get rights and content

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Cited by (14)

  • On the physical basis of a Larson-Miller constant of 20

    2018, International Journal of Pressure Vessels and Piping
    Citation Excerpt :

    This value of C is consistent with the result on aging obtained in Section 3 (C = 12.8). The value agrees also with the optimal values of C reported in the book [2]: C = 13 for creep crack initiation time in 10%Cr-Mo-W-VNbC cast steel at 550 and 600 °C [21], and C = 13.5 for in-reactor creep rupture life of 14%Cr-15%Ni-1.7%Mo-Ti austenitic stainless steel crept at 575 °C–750 °C [22]. Activation energy QLSD for lattice self-diffusion in a material is related to melting temperature TM of the material by Eq. (3), and varies from material to material.

  • Multiaxial thermomechanical creep-fatigue analysis of heat-resistant steels with varying chromium contents

    2014, International Journal of Fatigue
    Citation Excerpt :

    The variable loading conditions can shift the critical load to the fatigue domain by superimposed creep on the heated surface of components. Traditionally, creep-fatigue life has been assessed using the results of isothermal uniaxial tests conducted at (or close to) the peak operating temperature [1–5]. As one of the state-of-the-art creep-fatigue assessment procedures, comparison of crack initiation and propagation behavior under TMF (thermomechanical fatigue) and isothermal loading conditions on a modern 10%Cr steel was carried out in [6].

  • The influence of temperature transients on the lifetime of modern high-chromium rotor steel under service-type loading

    2013, Materials Science and Engineering: A
    Citation Excerpt :

    Temperature transients, constant or variable pressure in pressurized systems and constant or variable speed of turbine rotors produce a large variety of combined static and variable loading conditions. The pressure loading and centrifugal loading on rotors lead to quasi-static (primary) stress (Fig. 1) [1,2]. In addition, temperature transients cause strain cycling with variable thermal (secondary) stresses on the heated surfaces of turbine components.

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