Clauss, W. and Manfletti, Ch. and Sender, J. and Oschwald, M. and Fabelinsky, V. I. and Smirnov, V. V. and Stel'makh, O. M. and Vereschagin, K. A. (2010) Temperature Field in a Cryogenic LOX/CH4 Spray Flame. In: Proceedings of the 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference (AIAA 2010-7054). 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 25. - 28. July 2010, Nashville (TN), USA.
Full text not available from this repository.
To prepare for the application of CARS thermometry to LOX/methane spray flames CARS spectra have been recorded in a O2/CH4-burner at pressure up to 11 bar. Based on the experience obtained, potential probe molecules have been selected for the application of CARS to a LOX/CH4 spray flame. A CARS system allowing simultaneously the thermometry of the two probe molecules H2 and H2O was then used to map the temperature eld in a cryogenic rocket model combustor. The suitability of H2-CARS thermometry in a LOX/CH4 flame is demonstrated and the results provide a quantitative data base for the validation of simulation tools.
|Document Type:||Conference or Workshop Item (Speech, Paper)|
|Title:||Temperature Field in a Cryogenic LOX/CH4 Spray Flame|
|Journal or Publication Title:||Proceedings of the 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference|
|Keywords:||spray, flame, cryogenic, CARS|
|Event Title:||46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference|
|Event Location:||Nashville (TN), USA|
|Event Type:||international Conference|
|Event Dates:||25. - 28. July 2010|
|HGF - Research field:||Aeronautics, Space and Transport (old)|
|HGF - Program:||Space (old)|
|HGF - Program Themes:||W - no assignement|
|DLR - Research area:||Space|
|DLR - Program:||W - no assignement|
|DLR - Research theme (Project):||W -- no assignement (old)|
|Institutes and Institutions:||Institute of Space Propulsion > Raketenantriebe|
|Deposited By:||Michaela Hanke|
|Deposited On:||06 Dec 2010 16:50|
|Last Modified:||13 Dec 2010 12:20|
Repository Staff Only: item control page