Hydroxyl-Tagging-Velocimetry Measurements of a Supersonic Flow over a Cavity
Author:
Affiliation:
1. Vanderbilt University, Nashville, Tennessee 37235
2. U.S. Air Force Research Laboratory, Wright-Patterson Air Force Base, Ohio 45433
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.47264
Reference50 articles.
1. Cavity Flame-Holders for Ignition and Flame Stabilization in Scramjets: An Overview
2. Fundamental Studies of Cavity-Based Flameholder Concepts for Supersonic Combustors
3. Reattachment of a Compressible Turbulent Free Shear Layer
4. A study of compressible turbulent reattaching free shear layers
5. Supersonic Cavity Flows and Their Control
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