The effects of nozzle geometry upon sonic fuel injection as studied by OH-Flow-Tagging velocimetry
Author:
Affiliation:
1. Systems Research Laboratories, Inc., Dayton, OH
2. USAF, Aero Propulsion and Power Laboratory, Wright-Patterson AFB, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1991-575
Reference7 articles.
1. K. C. Schadow, E. Gutmark, K. J. Wilson, and R. A. Smith, "Multi-Step Dump Combustor Design to Reduce Combustion Instabilities," AIAA Paper 88-2854.
2. L. P. Goss, T. H. Chen, D. D. Trump, B. Sarka, and A. S. Nejad, "Flow Tagging Velocimetry Using the UV-Photodissociation of Water Vapor," AIAA Paper 91-0355.
3. Simultaneous multiple-point velocity measurements using laser-induced iodine fluorescence
4. Simultaneous planar measurements of velocity and pressure fields in gas flows using laser-induced fluorescence
5. Velocity visualization in gas flows using laser‐induced phosphorescence of biacetyl
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