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The effect of incomplete fuel-air mixing on the lean blowout limit, lean stability limit and no(x) emissions in lean premixed gas turbine combustors
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Shih, W.-P. Lee, J. G. Santavicca, D. A. |
| Copyright Year | 1994 |
| Description | Gas turbine engines for both land-based and aircraft propulsion applications are facing regulations on NOx emissions which cannot be met with current combustor technology. A number of alternative combustor strategies are being investigated which have the potential capability of achieving ultra-low NOx emissions, including lean premixed combustors, direct injection combustors, rich burn-quick quench-lean burn combustors and catalytic combustors. The research reported in this paper addresses the effect of incomplete fuel-air mixing on the lean limit performance and the NOx emissions characteristics of lean premixed combustors. |
| File Size | 162864 |
| Page Count | 4 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19950002749 |
| Archival Resource Key | ark:/13960/t2t48mm73 |
| Language | English |
| Publisher Date | 1994-11-01 |
| Access Restriction | Open |
| Subject Keyword | Inorganic And Physical Chemistry Combustion Chemistry Acoustic Measurement Chemical Effects Premixed Flames Gas Turbine Engines Fluorescence Pollution Monitoring Aircraft Engines Blowouts Noise Spectra Gas Mixtures Gas Composition Hydroxyl Emission Gas Turbines Combustion Stability Premixing Air Pollution Nitrogen Oxides Fuel Injection Combustion Chambers Exhaust Emission Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
