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The Global ETD Search service is a free service for researchers
to find electronic theses and dissertations. This service is
provided by the
Networked Digital Library of Theses and Dissertations.
Our metadata is collected from universities around the world. If you manage a university/consortium/country archive and want to be added, details can be found on the NDLTD website.
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Showing 11 to 20 of 280 (0.023 seconds)Spelling suggestions: "subject:"track growth"" "subject:"crack growth""
| 11 |
Correlation of mechanical test parameters with fatigue crack growth rates in structural steelsDivsalar, F. January 1988 (has links)
No description available.
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| 12 |
Mechanical properties of particle reinforced aluminaMorsi, Khaled M. B. E. January 1995 (has links)
No description available.
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| 13 |
Crack analysis by distributed strain nuclei with application to indentation testingLin, Shiann January 1997 (has links)
No description available.
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| 14 |
The application of the J-integral to stress corrosion crackingMackay, F. G. January 1987 (has links)
No description available.
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| 15 |
Detection of cracks in cylinders using modal analysisWake, Richard Neil January 1997 (has links)
No description available.
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| 16 |
Fatigue of aluminium-lithium alloysDudgeon, Helen D. January 1990 (has links)
No description available.
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| 17 |
An Innovative and Robust Approach to Studying Fatigue Properties of Aluminum 7075 Bar Utilizing Miniature I-Beam GeometryHynes, Wendy M. 11 July 2006 (has links)
Aerospace structures are optimally designed and analyzed to specifically-defined engineering parameters. Thus, there is a strong drive to understand fatigue properties of materials, enabling an engineer determine their influence on these constraints. Space structures are usually designed to minimize weight and volume; hence thin designs utilizing strong, lightweight materials are ultimately desired. The goal of this research is to address an innovative testing technique of material properties not readily obtained from current test methods. The properties studied in this research include crack growth rates of small diameter rods in both the radial and transverse grain directions under a constant-amplitude tensile load at room temperature. This approach is illustrated on I-beam specimen manufactured from Aluminum 7075-T7351 Bar. The crack growth rates from the experimental data are then compared with literature results for plates, sheets, and extrusions of the same material. The research completed reveals the test results have comparable [Paris relationship] exponential m-values. The significance of quantifying small diameter metallic material properties have potential for great impact on the future of space structures, but are not limited to one part of the industry.
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| 18 |
Finite element prediction of creep crack growth in three-dimensional components under mode 1 loadingSmith, S. D. January 1986 (has links)
No description available.
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| 19 |
The effect of environment on fatigue crack growth in 316 stainless steelNeailey, Kevin January 1987 (has links)
No description available.
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| 20 |
Stable crack growth in an aluminium-silicon bronze alloyPhoplonker, M. A. January 1987 (has links)
No description available.
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