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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 71 to 80 of 1320 (0.056 seconds)Spelling suggestions: "subject:"[een] STRUCTURAL ENGINEERING"" "subject:"[enn] STRUCTURAL ENGINEERING""
| 71 |
The mechanics of foams and honeycombsZhang, Junjie January 1989 (has links)
No description available.
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| 72 |
The wind induced vibration and fatigue of floating roofs on oil storage tanksRobinson, Nigel James January 1990 (has links)
No description available.
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| 73 |
Buckling of non-welded and welded aluminium columnsHong, G. M. January 1983 (has links)
No description available.
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| 74 |
Fatigue crack propagation in residual stress fieldsBraid, J. E. M. January 1982 (has links)
No description available.
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| 75 |
Crack growth at stress concentrationsShin, C.-S. January 1985 (has links)
No description available.
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| 76 |
Boundary-element stress analysis of thin and thick platesDebbih, Mohammed January 1989 (has links)
No description available.
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| 77 |
Failure of laminated fibre-reinforced composite structures subject to combined loadingsNahas, Mahmoud Nadim January 1980 (has links)
A new modified maximum strain failure criterion is proposed to predict the failure of the laminae of laminated fibre-reinforced composite structures when the laminate is subjected to combined loadings. The new criterion takes into account the layer non-linear behaviour which is an important factor in the failure prediction operation. The analysis of laminated structures containing laminae with non-linear stress-strain response is also studied and a new method is proposed for this analysis. The modified failure criterion introduces two levels of failure. The lower level is of the lamina degradation, above which the lamina will exhibit irreversible damage. The higher failure level, however, is associated with the “ultimate” failure of the lamina, above which the lamina cannot sustain any load. After the “ultimate” failure of a lamina in a certain direction, the post-failure model proposed in this study assumes the failed layer to unload in the failed direction only following a decreasing exponential function where the secant modulus decreases gradually to zero. The theoretical results are compared with experimental results obtained from tests carried out on tubular composite specimens under combined loading conditions. Acoustic emission, C-scanning and photomicrographic tests were also conducted to examine the damage caused when the linear limit is exceeded. The cylindrical specimens used in the experimental investigation introduced two additional problems which are also studied here. These are the design of the tubular test specimens, and the buckling of cylindrical shells under combined loading. Comprehensive survey of the previous theories for all the problems studied in this thesis is presented, and where possible, the results obtained by previous investigators are compared with the present proposed solutions and commented on.
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| 78 |
Assessment of fire damage to concrete structuresMacGregor Smith, L. January 1983 (has links)
No description available.
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| 79 |
Bearing capacity of unreinforced and reinforced soil under rapid loadingQayyum, Tanvir Iqbal January 1995 (has links)
No description available.
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| 80 |
The stability of revetment blockwork under wave actionYuwono, Nur January 1990 (has links)
No description available.
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