Experiments on Oblique Shock Interactions with Planar Mixing Regions
Author:
Affiliation:
1. University of Queensland, Queensland 4072, Australia
2. University of Oxford, Oxford OX1 3PJ, England, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.26
Reference13 articles.
1. Shock-wave-induced mixing enhancement in scramjet combustors
2. Turbulence measurements for heated gas slot injection in supersonic flow
3. Exploratory study of turbulent structure of a compressible shear layer using fluctuating pitot pressure measurements
4. Investigation of a contoured wall injector for hypervelocity mixing augmentation
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1. Irregular self-similar configurations of shock-wave impingement on shear layers;Journal of Fluid Mechanics;2019-06-14
2. Interaction of Oblique Shocks and Laminar Shear Layers;AIAA Journal;2018-03
3. High bandwidth stagnation temperature measurements in a Mach 6 gun tunnel flow;Experimental Thermal and Fluid Science;2003-02
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