Planar OH density and apparent temperature measurements in a supersonic combusting flow
Author:
Affiliation:
1. University of Virginia, Charlottesville, Virginia 22903
2. Princeton University, Princeton, New Jersey 08544
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.13090
Reference20 articles.
1. McDaniel, J., Fletcher, D., Hartfield, R., Jr., and Hollo, S. "Staged Transverse Injection into Mach 2 Flow Behind a Rearward-Facing Step: A 3-D Compressible Test Case for Hypersonic Combustor Code Validation," AIAA Paper 91-5071, Dec.1991.
2. Two-dimensional imaging of OH laser-induced fluorescence in a flame
3. Method for measuring temperatures and densities in hypersonic wind tunnel air flows using laser-induced O_2 fluorescence
4. Nitric oxide measurements in a flame by laser fluorescence
5. Simultaneous measurements of velocity, temperature, and pressure using rapid cw wavelength-modulation laser-induced fluorescence of OH
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