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Aircraft engine systems
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Veres, Joseph |
| Copyright Year | 2001 |
| Description | This report outlines the detailed simulation of Aircraft Turbofan Engine. The objectives were to develop a detailed flow model of a full turbofan engine that runs on parallel workstation clusters overnight and to develop an integrated system of codes for combustor design and analysis to enable significant reduction in design time and cost. The model will initially simulate the 3-D flow in the primary flow path including the flow and chemistry in the combustor, and ultimately result in a multidisciplinary model of the engine. The overnight 3-D simulation capability of the primary flow path in a complete engine will enable significant reduction in the design and development time of gas turbine engines. In addition, the NPSS (Numerical Propulsion System Simulation) multidisciplinary integration and analysis are discussed. |
| File Size | 971788 |
| Page Count | 22 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20010108903 |
| Archival Resource Key | ark:/13960/t5w71dp4w |
| Language | English |
| Publisher Date | 2001-06-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Three Dimensional Flow Temperature Inversions Cost Reduction Turbofan Engines Computerized Simulation Aircraft Engines Combustion Chambers Design Analysis Three Dimensional Models Systems Integration Propulsion System Configurations Computer Programs Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
