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The overall goal is to develop a structural model that enables configuration of different jet engine concepts and used as input to the research project where dynamic and stress analysis will be performed. The specific goal is to: use the KBE-module of Siemens PLM NX5 called Knowledge Fusion to implement a simplified turbofan jet engine containing accordin to Figure 1. Although the focus is on the structural (i.e the parts that create the stiffness of the jet engine and mostly are static) parts ther isa na interest to model the fan and the shaft as the masses will be needed as input to the research project.
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