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Application of a real-fluid turbomachinery analysis to rocket turbopump geometries
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Sondak, Douglas L. Dorney, Daniel J. Marcu, Bogdan |
| Copyright Year | 2005 |
| Description | 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. |
| File Size | 10637943 |
| Page Count | 10 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20050092365 |
| Archival Resource Key | ark:/13960/t8sb92432 |
| Language | English |
| Publisher Date | 2005-01-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Thermodynamics Navier-stokes Equation Incompressible Flow Turbine Pumps Three Dimensional Flow Flow Distribution Rocket Engines Turbomachinery Turbines Compressible Flow Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
