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Pump cfd code validation tests
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Brozowski, L. A. |
| Copyright Year | 1993 |
| Description | Pump CFD code validation tests were accomplished by obtaining nonintrusive flow characteristic data at key locations in generic current liquid rocket engine turbopump configurations. Data were obtained with a laser two-focus (L2F) velocimeter at scaled design flow. Three components were surveyed: a 1970's-designed impeller, a 1990's-designed impeller, and a four-bladed unshrouded inducer. Two-dimensional velocities were measured upstream and downstream of the two impellers. Three-dimensional velocities were measured upstream, downstream, and within the blade row of the unshrouded inducer. |
| File Size | 1105827 |
| Page Count | 30 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19940022094 |
| Archival Resource Key | ark:/13960/t13n72t4q |
| Language | English |
| Publisher Date | 1993-12-15 |
| Access Restriction | Open |
| Subject Keyword | Mechanical Engineering Turbine Pumps Laser Doppler Velocimeters Computational Fluid Dynamics Flow Distribution Flow Velocity Velocity Distribution Liquid Propellant Rocket Engines Program Verification Computers Pump Impellers Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
