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Time-dependent simulations of incompressible flow in a turbopump using overset grid approach
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Kiris, Cetin Kwak, Dochan |
| Copyright Year | 2001 |
| Description | This viewgraph presentation provides information on mathematical modelling of the SSME (space shuttle main engine). The unsteady SSME-rig1 start-up procedure from the pump at rest has been initiated by using 34.3 million grid points. The computational model for the SSME-rig1 has been completed. Moving boundary capability is obtained by using DCF module in OVERFLOW-D. MPI (Message Passing Interface)/OpenMP hybrid parallel code has been benchmarked. |
| File Size | 689740 |
| Page Count | 14 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20020052629 |
| Archival Resource Key | ark:/13960/t45q9w255 |
| Language | English |
| Publisher Date | 2001-01-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Thermodynamics Time Dependence Incompressible Flow Turbine Pumps Simulation Space Shuttle Main Engine Mathematical Models Boundaries Computational Grids Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
