Development of a Dual-Pump CARS System for Measurements in a Supersonic Combusting Free Jet
Author:
Affiliation:
1. George Washington University
2. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2012-1193
Reference45 articles.
1. Simultaneous coherent anti-Stokes Raman spectroscopy measurements inhydrogen-fueled supersonic combustion
2. Multiplex CARS measurements in supersonic H2/air combustion
3. Coherent Anti-Stokes Raman Spectroscopic Thermometry in a Supersonic Combustor
4. Three-laser coherent anti-Stokes Raman scattering measurements of two species
5. Dual-Pump Coherent Anti-Stokes Raman Scattering Measurements in a Supersonic Combustor
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1. Miniaturized Combustor for Supersonic Methane–Air Flames;Journal of Propulsion and Power;2014-09
2. Large-Eddy/Reynolds-Averaged Navier–Stokes Simulations of Reactive Flow in Dual-Mode Scramjet Combustor;Journal of Propulsion and Power;2014-05
3. Dual-Pump Coherent Anti-Stokes Raman Spectroscopy Measurements in a Dual-Mode Scramjet;Journal of Propulsion and Power;2014-05
4. Measurement of Vibrational Nonequilibrium in a Supersonic Freestream Using Dual-Pump CARS;28th Aerodynamic Measurement Technology, Ground Testing, and Flight Testing Conference;2012-06-25
5. Dual-Pump CARS Measurements in the University of Virginia's Dual-Mode Scramjet: Configuration "A";50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2012-01-09
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