Fatigue '96: Proceedings of the 6th International Fatigue Congress
The aim of the 6th International Fatigue Congress, besides covering the entire field of fatigue, was to promote the intimate connection between basic science and engineering application by the selection of appropriate session topics.Fatigue is the main cause of failure of engineering structures and components. Making reliable fatigue predictions is highly difficult because knowledge about fatigue mechanisms in all stages of the fatigue process must be developed much further. In addition, the decreasing availability of raw materials and energy resources forces engineers to continually reduce the weight of constructions. This congress presents research results also particularly for new materials, including composites. Researchers, on the other hand, are confronted with the engineering demands. Futhermore, the overwhelming development which is presently taking place in the field of computer software and hardware dealing with fatigue problems is outlined along with the directions of future developments in all areas of fatigue.Close to 300 fully peer-reviewed papers are published in the proceedings, including nearly 30 overview and keynote papers covering the various session topics. The proceedings should therefore serve as a comprehensive review of the fatigue field at the present state-of-the-art, suitable for scientists, engineers and students.
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BEEVERS MEMORIAL LECTURE
ADVANCED FATIGUE PROPERTIES OF METAL MATRIX
Effects of Surface Crack Length and 1391
80 other sections not shown
austenitic bicrystals calculated constant amplitude copper corrosion crack closure crack growth rate crack length crack opening stress crack tip cyclic deformation cyclic hardening cyclic stress-strain da/dN decrease dislocation structure effective stress Engng equation experimental fatigue crack growth fatigue crack initiation fatigue crack propagation fatigue damage fatigue limit fatigue lives fatigue strength fatigue tests ferrite fracture mechanics fracture surface frequency grain boundary hysteresis loop increase interface investigated KEYWORDS Kmax loading conditions long crack low cycle fatigue material mean stress metals microcracks microstructure mode Mughrabi number of cycles observed orientation parameters pearlite phase plane plane strain plastic deformation plastic strain amplitude plastic zone prediction range regime S-N curve shape memory alloy short cracks shown in Fig shows single crystals slip bands small cracks small fatigue cracks stage stainless steel strain rate stress amplitude stress intensity factor stress level stress-strain curves tensile threshold vacuum values