Article | REF: B4181 V1

Turbomachinery: calculating compressible flows

Author: Georges MEAUZÉ

Publication date: November 10, 1995, Review date: July 5, 2018 | Lire en français

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    2. Viscosity of flow

    Viscosity naturally plays a key role in turbomachinery, as it is the main source of losses. These losses are usually classified into three categories:

    • profile losses, linked to the development of viscous layers on the blades and the wakes they create, which are all the more sheared the greater the three-dimensional warping effect mentioned above;

    • secondary losses, which appear at the edges of the blades and give rise to significant vortices, as a result of the viscous flow being deflected onto the hub and casing. It should be noted here that the appearance of the main vortices is not a purely viscous phenomenon, but results from the heterogeneous velocity profile at the impeller inlet. Non-viscous calculations clearly demonstrate this behavior qualitatively;

    • losses due to...

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