| 1. | Mascotte, a cryogenic combustion research test bench - ONERA / DEFA-EN |
| | Low pressure combustor... High pressure combustor... |
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| 2. | Publications - ONERA / DEFA |
| | Dumand C., Sabel'nikov V., The effect of micromixing on combustion extinction limits for micro combustor applications - 30th International Symposium on Combustion - 2004, Chicago... Dumand C., Sabel'nikov V., The effect of micromixing on combustion extinction limits for micro combustor application - - 6th International Symposium on Engineering Turbulence modelling and Measurement - - 2005, Sardinia... |
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| 3. | A cryogenic combustion research test bench - Operation with Oxygen / Hydrogen - ONERA / DEFA-EN |
| | The present version of Mascotte can reach 80 bar with adapted combustor and nozzle.... |
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| 4. | Publications - ONERA / DEFA-EN |
| | Dumand C., Sabel'nikov V., The effect of micromixing on combustion extinction limits for micro combustor applications - 30th International Symposium on Combustion - 2004, Chicago... Dumand C., Sabel'nikov V., The effect of micromixing on combustion extinction limits for micro combustor application - - 6th International Symposium on Engineering Turbulence modelling and Measurement - - 2005, Sardinia... |
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| 5. | Flow in a Combustion Chamber - ONERA's Science Pictures |
| | Flow in a combustion chamberTomographic image of Mie scattering on the A3C combustor. Pictures. |
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| 6. | Transatmospheric Aircraft (AHYP1) |
| | Like a ramjet, it compresses the air simply by slowing it down in the air intake, but the speed remains supersonic at the combustor inlet and throughout the engine, which is why this type of engine is called scramjet (for supersonic combustion ramjet).... Research is essentially focused on the fuel injection system (usually hydrogen) and the combustor.... |
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| 7. | uftz3w6s.PDF |
| | 9h00 Potential applications of Plasma on jet engines combustors M. Cazalens (SNECMA) 9h30 Flame stabilisation using plasmas P. Vervisch (CORIA) 10h00 The properties of the streamer microwave discharge and its influence on a supersonic flowfield around body K. Khodataev (Moscow Radiotechnical Institute) 10h30 - 10h50 Coffee Break 10h50 Jet breakup control T. Poinsot (IMFT) 11h20 A New Plasma Catalysis Approach for Hydrocarbons Conversion, Flame Ignition and Control B. Potapkin (Kurchatov Institute) 11h50 Non-intrusive laser measurement tools J.P. Taran (ONERA) 12h20 - 14h00 Lunch Afternoon session :... |
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| 8. | presentation SMSMEO ONERA KLOTZ [ Lecture seule ] |
| | This work was supported by european project INTELLECT D.M (Integrated Lean Low-Emission Combustor Design Methodology) which has the objective to develop a design methodology for combustors in order to reduce pollutant emission.... Combustor chamber... |
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| 9. | 29-Geigle.pdf |
| | One of the contained tasks is dealing with application of laserinduced incandescence (LII) as a tool to determine soot distributions inside the combustor quantitatively.... Trends are presented showing soot distributions upon changes of the combustor operating conditions between 4 and 23 bars at realistic geometries and flow rates.... |
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| 10. | 14-Matuszewski.pdf |
| | Keywords : multi-point combustor, pollutant formation, NOx emission, turbulent combustion, lagrangian combustion model.... The first idea was to create Dual Annular Combustor (DAC) [ 1, 2, 3 ] including two injections heads, one dedicated to high power operating conditions, the other dedicated to idle or low power operating conditions.... |
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