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- W109600807 abstract "In this study, we examine the effect of the critical geometric features and interface conditions in the dovetail region of aeroengine disc assemblies upon the contact stress distribution at the blade/disc interface. Three aspects of the work are accordingly examined. The first is concerned with the finite element modelling and analysis of the contact stress field. The second is concerned with the assessment of the mechanical integrity and the damage tolerance capability and the “least damage” potential of the examined blade/disc configurations. The third is devoted to the difficulties associated with the use of user-defined contact stiffness parameters. To overcome these difficulties, we propose a new method, which is mathematically consistent and accurate, known as variational inequalities (VI). The outcome of the work reveals: (i) the significant effect of the different geometric features and interface conditions on the resulting contact stresses, (ii) the ability to predict the crack propagation with reasonable accuracy, and (iii) the advantages of the newly developed VI modelling technique." @default.
- W109600807 created "2016-06-24" @default.
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- W109600807 date "2000-01-01" @default.
- W109600807 modified "2023-09-25" @default.
- W109600807 title "ON THE MECHANICAL INTEGRITY OF AEROENGINE COMPRESSOR DISC ASSEMBLIES" @default.
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- W109600807 doi "https://doi.org/10.1016/b978-008043711-8/50017-9" @default.
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