IHS ESDU Effect of environment on fatigue crack propagation in aluminium alloy sheet and plate. 88007

Description
ESDU 88007 gives graphs of rate of increase in crack length per loading cycle plotted against stress intensity factor range for 10 alloys, many with various heat treatments. The data were extracted from the literature and relate to various environments including dry or humid air, water, salt water or salt water spray. The specimens tested were from sheet, clad sheet, or plate and range from 0.04 to 4.49 in (1 to 114 mm) thick. Full details of the environments and tests are tabulated together with details of the specimens such as tensile strength, proof stress and composition. Included with the curves is a table giving the constants for the Paris equations that describe them. Discussion of the results considers the influence of environment, heat treatment, and stress ratio on the crack growth rate.
Description
ESDU 88007 gives graphs of rate of increase in crack length per loading cycle plotted against stress intensity factor range for 10 alloys, many with various heat treatments. The data were extracted from the literature and relate to various environments including dry or humid air, water, salt water or salt water spray. The specimens tested were from sheet, clad sheet, or plate and range from 0.04 to 4.49 in (1 to 114 mm) thick. Full details of the environments and tests are tabulated together with details of the specimens such as tensile strength, proof stress and composition. Included with the curves is a table giving the constants for the Paris equations that describe them. Discussion of the results considers the influence of environment, heat treatment, and stress ratio on the crack growth rate.

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Effect of environment on fatigue crack propagation in aluminium alloy sheet and plate. - 88007 - IHS ESDU
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Effect of environment on fatigue crack propagation in aluminium alloy sheet and plate.
88007
Effect of environment on fatigue crack propagation in aluminium alloy sheet and plate. 88007
ESDU 88007 gives graphs of rate of increase in crack length per loading cycle plotted against stress intensity factor range for 10 alloys, many with various heat treatments. The data were extracted from the literature and relate to various environments including dry or humid air, water, salt water or salt water spray. The specimens tested were from sheet, clad sheet, or plate and range from 0.04 to 4.49 in (1 to 114 mm) thick. Full details of the environments and tests are tabulated together with details of the specimens such as tensile strength, proof stress and composition. Included with the curves is a table giving the constants for the Paris equations that describe them. Discussion of the results considers the influence of environment, heat treatment, and stress ratio on the crack growth rate.

ESDU 88007 gives graphs of rate of increase in crack length per loading cycle plotted against stress intensity factor range for 10 alloys, many with various heat treatments. The data were extracted from the literature and relate to various environments including dry or humid air, water, salt water or salt water spray. The specimens tested were from sheet, clad sheet, or plate and range from 0.04 to 4.49 in (1 to 114 mm) thick. Full details of the environments and tests are tabulated together with details of the specimens such as tensile strength, proof stress and composition. Included with the curves is a table giving the constants for the Paris equations that describe them. Discussion of the results considers the influence of environment, heat treatment, and stress ratio on the crack growth rate.

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Technical Specifications

  IHS ESDU
Product Category Standards and Technical Documents
Product Number 88007
Product Name Effect of environment on fatigue crack propagation in aluminium alloy sheet and plate.
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