Coherent Anti-Stokes Raman Spectroscopic Thermometry in a Supersonic Combustor
Author:
Affiliation:
1. George Washington University, Hampton, Virginia 23681
2. NASA Langley Research Center, Hampton, Virginia 23681
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.6844
Reference27 articles.
1. 1Cutler, A. D., Danehy, P. M., Springer, R. R., DeLoach, R., and Capriotti, D. P. “CARS Thermometry in a Supersonic Combustor for CFD Code Validation,” AIAA Paper 2002-0743, Jan. 2002.
2. Fundamental Mixing and Combustion Experiments for Propelled Hypersonic Flight
3. An experimental and CFD study of a supersonic coaxial jet
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