Keywords (Extracted from title, table of contents and
abstract of thesis) Analysis, Crack, Propagation,
Thick-Walled, Cylinder, Fatigue, Loading,
industries, engineering, threshold |
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Abstract Reliability of
materials and structures in the form of thick-walled cylinders is of
critical importance to many industries including power, nuclear,
chemical, armament, and food processing industries. Catastrophic
failure of these cylinders can put the human life and the
surroundings at very high risk. For this reason, the integrity of
the cylinder should be guaranteed. The integrity of nearly all
engineering structures is threatened by the presence of cracks.
Structural failure occurs if a crack larger than a critical size
exists. Although most well designed structures initially contain no
critical cracks, sub critical cracks can grow to failure under
fatigue loading, called fatigue crack propagation. Fatigue failure
that is failure under repeated or cyclic loading is a serious
concern of engineering design. Under fatigue loading the component
may fail at a stress level that is far below its yield strength. In
present research the fatigue crack propagation, in a thick-walled
cylinder, is analyzed through detailed experimental work and finite
element analysis and the fatigue crack growth life of the cylinder,
with crack at the bore surface, has been predicted.
Extrusion process induces micro structural anisotropy in the
thick-walled cylinder. The intensive experimental work, with the
help of laboratory tests on the material under investigation,
explores the details of the material and the
microstructure-properties relationship in the longitudinal and
transverse orientations. The yield and tensile strength in two
orientations are not significantly different. However, percent
elongation, reduction in area, impact strength and fracture
toughness of the material are superior in the axial direction. A
marked impact of anisotropy is found on the fatigue properties and
shorter fatigue life in the transverse direction was obtained, which
is 41 to 62 % lower in the tested stress range of 129 to 47 MPa. The
theoretical part of the study includes modeling and simulation based
on finite element method and the numerical technique is employed for
the simulation of fatigue crack propagation. The finite element
analysis, based on linear elastic fracture mechanics (LEFM) combined
with the Paris law, suitably predicts the fatigue life and provides
the results that are in good agreement with the experimental
results. Both the experimental and numerical results of the crack
growth data at different stress levels were found in good agreement
all along the Paris regime. In the near threshold region the
predicted values are conservative. With implementation of the
present scheme of work the fatigue crack growth life of the
thick-walled cylinder, with internal axial crack, has been
predicted.
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