A rapid viscous-inviscid interaction method for the preliminary design of s-shaped transition ducts

For preliminary design of compressor transition ducts, knowledge-based tools for the rapid assessment of aerodynamic performance of S-shaped ducts are not currently available in the open literature. This is due to the highly complex flow developing under the combined influence of pressure gradients...

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Bibliographic Details
Main Authors: Alan Veyrat, Jon Carrotte, Duncan Walker, C Hall, H Simpson
Format: Default Conference proceeding
Published: 2021
Subjects:
separation
flow deviation
loading
composite law-of-the-wall
integral method
parametric splines
streamline curvature
Online Access:https://hdl.handle.net/2134/16780063.v1
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https://hdl.handle.net/2134/16780063.v1

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