LIBROS DEL AUTOR: reising dr steffen

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  • Transonic Compressor Stages with Non-Axisymmetric End Walls
    Reising Dr. Steffen
    The development of axial aircraft compressors has led to high stage loadings and therewith reductions in entire engine size and weight. This trend also promotes several disadvantages such as the risks of flow separation and higher secondary flows that are associated with increased stage loading. The application of non-axisymmetric end walls is one approach to reduce blade loadi...
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