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The e3 combustors: status and challenges. [energy efficient turbofan engines
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Rohde, J. E. Sokolowski, D. E. |
| Copyright Year | 1981 |
| Description | The design, fabrication, and initial testing of energy efficient engine combustors, developed for the next generation of turbofan engines for commercial aircraft, are described. The combustor designs utilize an annular configuration with two zone combustion for low emissions, advanced liners for improved durability, and short, curved-wall, dump prediffusers for compactness. Advanced cooling techniques and segmented construction characterize the advanced liners. Linear segments are made from castable, turbine-type materials. |
| File Size | 2027488 |
| Page Count | 25 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19810019557 |
| Archival Resource Key | ark:/13960/t9n34p634 |
| Language | English |
| Publisher Date | 1981-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Engine Design Linings Combustion Products Cooling Systems Fuel Consumption Turbofan Engines Engine Tests Aircraft Engines Combustion Chambers Annular Flow Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
