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Three-dimensional euler time accurate simulations of fan rotor-stator interactions
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Boretti, A. A. |
| Copyright Year | 1990 |
| Description | A numerical method useful to describe unsteady 3-D flow fields within turbomachinery stages is presented. The method solves the compressible, time dependent, Euler conservation equations with a finite volume, flux splitting, total variation diminishing, approximately factored, implicit scheme. Multiblock composite gridding is used to partition the flow field into a specified arrangement of blocks with static and dynamic interfaces. The code is optimized to take full advantage of the processing power and speed of the Cray Y/MP supercomputer. The method is applied to the computation of the flow field within a single stage, axial flow fan, thus reproducing the unsteady 3-D rotor-stator interaction. |
| File Size | 1352925 |
| Page Count | 32 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19910014811 |
| Archival Resource Key | ark:/13960/t18m26w52 |
| Language | English |
| Publisher Date | 1990-12-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Conservation Equations Computational Fluid Dynamics Interactional Aerodynamics Rotor Stator Interactions Computer Systems Performance Unsteady Flow Computer Programs Rotor Dynamics Time Dependence Three Dimensional Flow Euler Equations of Motion Flow Distribution Unsteady Aerodynamics Stators Tvd Schemes Computational Grids Cray Computers Axial Flow Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |