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Enhancing aeropropulsion research with high-speed interactive computing
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Szuch, John R. Arpasi, Dale J. Strazisar, Anthony J. |
| Copyright Year | 1991 |
| Description | NASA-Lewis has committed to a long range goal of creating a numerical test cell for aeropropulsion research and development. Efforts are underway to develop a first generation Numerical Propulsion System Simulation (NPSS). The NPSS will provide a unique capability to numerically simulate advanced propulsion systems from nose to tail. Two essential ingredients to the NPSS are: (1) experimentally validated Computational Fluid Dynamics (CFD) codes; and (2) high performing computing systems (hardware and software) that will permit those codes to be used efficiently. To this end, NASA-Lewis is using high speed, interactive computing as a means for achieving Integrated CFD and Experiments (ICE). The development is described of a prototype ICE system for multistage compressor flow physics research. |
| File Size | 9171461 |
| Page Count | 18 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19910015482 |
| Archival Resource Key | ark:/13960/t4rj9c41g |
| Language | English |
| Publisher Date | 1991-01-01 |
| Access Restriction | Open |
| Subject Keyword | Turbocompressors Propulsion System Performance Computational Fluid Dynamics Computer Systems Performance Air Breathing Engines Computerized Simulation Systems Simulation Computer Systems Programs Propulsion System Configurations Parallel Processing Computers Program Verification Computers Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
