Effect of plate thickness on the in-plane and through-thickness stresses at a hole /
Holes exist in metallic aircraft structures for either design or construction reasons and their stress concentrating effect is such that they are common regions of fatigue crack initiation. A combined experimental and numerical study has been carried out to examine the influence of thickness on the...
Guardado en:
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| Autores Corporativos: | , |
| Formato: | Libro |
| Lenguaje: | English |
| Publicado: |
Melbourne :
DSTO Aeronautical and Maritime Research Laboratory,
1996.
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| Colección: | Technical report (Defence Science and Technology Organisation (Australia)) ;
DSTO-TR-0330. |
| Materias: | |
| Acceso en línea: | http://www.dsto.defence.gov.au/corporate/reports/DSTO-TR-0330.pdf |
| Sumario: | Holes exist in metallic aircraft structures for either design or construction reasons and their stress concentrating effect is such that they are common regions of fatigue crack initiation. A combined experimental and numerical study has been carried out to examine the influence of thickness on the surface and through-thickness stress distributions of aluminimum alloy specimens with central holes. Thermographic and strain-guarge measurements were made on several thicknesses of specimens, the central holes of which were either reamed of cold-exapnded by 3.6%. The experimental results were compared with those from numerical analyses of the specimens by three-dimensional finite-element modelling. |
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| Notas: | "AR No. AR-009-683"--T.p. verso. |
| Descripción Física: | 24 p. : ill. ; 30 cm. |
| Bibliografía: | Includes bibliographical references (p. 21) |