Abstract
The paper presents the results of a full-assembly three-dimensional Navier-Stokes calculation of a typical s-shaped transition duct configuration of short axial length and huge radial slope in front of a modern high-pressure compressor. The investigated duct has got nine thin and one thick strut followed by a row of forty HPC inlet guide vanes. The results give an understanding of the three-dimensional flow field around the struts and the interaction of the struts with the HPC inlet guide vanes. A comparison to two-dimensional calculations and test results is provided where available and shows the suitability of the used method for the duct design.
| Original language | English |
|---|---|
| State | Published - 2005 |
| Externally published | Yes |
| Event | 6th Conference on Turbomachinery: Fluid Dynamics and Thermodynamics, ETC 2005 - Lille, France Duration: 7 Mar 2005 → 11 Mar 2005 |
Conference
| Conference | 6th Conference on Turbomachinery: Fluid Dynamics and Thermodynamics, ETC 2005 |
|---|---|
| Country/Territory | France |
| City | Lille |
| Period | 7/03/05 → 11/03/05 |
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