A three-dimensional flow solver has been developed for turbomachinery components utilizing real fluid properties. The code is applicable to both incompressible and compressible flow fields. In this study, the code has been applied to the analysis of inducer and impeller geometries representative of those used in rocket engine applications. The predicted results show good agreement with the available experimental data.
Application of a Real-Fluid Turbomachinery Analysis to Rocket Turbopump Geometries
AIAA 43rd Aerospace Sciences Meeting and Exhibit ; 2005 ; Reno, NV, United States
2005-01-01
Preprint
No indication
English
Application of a Real-Fluid Turbomachinery Analysis to Rocket Turbopump Geometries
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