OH Planar Laser-Induced Fluorescence Velocity Measurements in a Supersonic Combustor
Author:
Affiliation:
1. University of Virginia, Charlottesville, Virginia 22903
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.157
Reference13 articles.
1. Evaluation of parallel injector configurations for Mach 2 combustion
2. Facility opportunities and associated stream chemistry considerations for hypersonic air-breathing propulsion
3. A clean air continuous flow propulsion facility
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