Turbomachinery Schema

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Turbomachinery Schema

The geometry of a turbomachinery model can be quite complex, but all these models have some characteristics in common, such as the presence of one or more components, and parts that play the role of inlet, outlet, fluid domain, hub or shroud for each component. While some turbomachinery simulations are run for the entirely of the geometry, it is more common that a model will represent only a section of the 360 degrees total geometry (often refereed to as wedge), and that a rotational symmetry needs to be applied in order to reconstruct the entire model.
All of this information is crucial when running turbomachinery specific analysis. In EnSight, the user can provide the information manually by entering them into the Initialization section of the Turbomachinery tool (see the Turbomachinery section in the User Manual for more details). This information is then stored into EnSight's parts and case METADATA for future use. Some readers have the ability to automatically detect these settings and fill in the METADATA information directly, resulting in a more streamlined experience for the user. Here we will present and explain each of the METADATA information that is needed for Turbomachinery analysis.

On the METDATA for the ENS_CASE object, set:


On METADATA for the ENS_PART objects, set: