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Laboratory studies of lean combustion
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Angeli, J. W. Oppenheim, A. K. Pitz, R. W. Sawyer, R. F. Schefer, R. W. Ganji, A. R. Daily, J. W. |
| Copyright Year | 1977 |
| Description | The fundamental processes controlling lean combustion were observed for better understanding, with particular emphasis on the formation and measurement of gas-phase pollutants, the stability of the combustion process (blowout limits), methods of improving stability, and the application of probe and optical diagnostics for flow field characterization, temperature mapping, and composition measurements. The following areas of investigation are described in detail: (1) axisymmetric, opposed-reacting-jet-stabilized combustor studies; (2) stabilization through heat recirculation; (3) two dimensional combustor studies; and (4) spectroscopic methods. A departure from conventional combustor design to a premixed/prevaporized, lean combustion configuration is attractive for the control of oxides of nitrogen and smoke emissions, the promotion of uniform turbine inlet temperatures, and, possibly, the reduction of carbon monoxide and hydrocarbons at idle. |
| File Size | 829775 |
| Page Count | 20 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19780003136 |
| Archival Resource Key | ark:/13960/t9b61cd4p |
| Language | English |
| Publisher Date | 1977-10-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Combustion Physics Gas Turbines Exhaust Gases Pollution Control Hydrocarbons Combustion Products Nitrogen Oxides Aircraft Engines Fuel-air Ratio Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |