PLIF imaging measurements compared to model calculations in high-temperature Mach 3 airflow over a sphere
Author:
Affiliation:
1. Physical Sciences, Inc., Andover,MA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1993-92
Reference19 articles.
Cited by 8 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. NO PLIF imaging in the CUBRC 48-inch shock tunnel;Experiments in Fluids;2012-09-15
2. NO PLIF Imaging in the CUBRC 48" Shock Tunnel;49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2011-01-04
3. Velocimetry and Thermometry of Supersonic Flow Around a Cylindrical Body;AIAA Journal;1998-06
4. Comparison of calculated and measured temperature fields in the AEDC Impulse Facility;Advanced Measurement and Ground Testing Conference;1996-06-17
5. Comparison of planar fluorescence measurements and computational modeling of shock-layer flow;AIAA Journal;1996-03
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