Visualization and Thermometry in Hypersonic Wedge and Leading-Edge Separated Flows
Author:
Affiliation:
1. University of New South Wales
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2017-0443
Reference22 articles.
1. A study of the free-piston shock tunnel.
2. Planar laser-fluorescence imaging of combustion gases
3. Temporally resolved, two-line fluorescence imaging of NO temperature in a transverse jet in a supersonic cross flow
4. Multi-line fluorescence imaging of the rotational temperature field in a shock-tunnel free jet
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