Laser-induced iodine fluorescence technique for quantitative measurement in a nonreacting supersonic combustor
Author:
Affiliation:
1. University of Virginia, Charlottesville, Virginia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.10148
Reference18 articles.
1. Survey of supersonic combustion ramjet research at Langley
2. Supersonic‐nitrogen flow‐field measurements with the resonant Doppler velocimeter
3. Laser-induced fluorescence visualization on supersonic mixing nozzles that employ gas-trips
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