Creep-fatigue life evaluation of high chromium ferritic steel under non-proportional loading
Journal Title: Frattura ed Integrità Strutturale - Year 2016, Vol 10, Issue 38
Abstract
T Multiaxial creep-fatigue tests under non-proportional loading conditions with various strain rates were carried out using a hollow cylinder specimen of a high chromium ferritic steel at 823K in air to discuss the influence of non-proportional loading on failure life. Strain paths employed were a push-pull loading and a circle loading. The push-pull loading test is proportional strain path test. The circle loading test is non-proportional strain path test in which sinusoidal waveforms of axial and shear strains have 90 degree phase difference. The failure life is affected largely by the strain rate and the non-proportional loading. This paper presents a modified strain range for life evaluation considering the strain rate based on a non-proportional strain parameter proposed by authors. The strain range is a suitable parameter for life evaluation of tested material under non-proportional loading at high temperature
Authors and Affiliations
T. Morishita, Y. Murakami , H. Tanigawa
Damage propagation in a masonry arch subjected toslow cyclic and dynamic loadings
In the present work, the damage propagation of a masonry arch induced by slow cyclic anddynamic loadings is studied. A two-dimensional model of the arch is proposed. A nonlocal damage-plasticconstitutive law is ado...
Crack simulation models in variable amplitude loading - a review
This work presents a review of crack propagation simulation models considering plane stress and plane strain conditions. It is presented also a chronological different methodologies used to perform the crack ...
Fracture mechanics analyses of the slip-side joggle regions of wing-leading-edge panels
The Space Shuttle wing-leading edge consists of panels that are made of reinforced carbon-carbon. Coating spallation was observed near the slip-side region of the panels that experience extreme heating. To understand t...
Failure analysis of dissimilar single-lap joints
Single-lap joints made of aluminium and carbon fibre adherends of different thickness are tested to understand better the behaviour of such dissimilar joints. The overlap length and the thickness of the adhesive&n...
Characterization of fracture properties of thin aluminum inclusions embedded in anisotropic laminate composites
The fracture properties of thin aluminum inclusions embedded in anisotropic paperboard composites, of interest for food and beverage packaging industry, can be determined by performing tensile tests on non-conventi...