Effect of boundary layer thickness on transverse sonic jet mixing in a supersonic turbulent crossflow
Author:
Affiliation:
1. Engineering Research and Development, TRUMPF North America, Cranbury, New Jersey 08512, USA
2. Department of Mechanical Engineering, Lafayette College, Easton, Pennsylvania 18042, USA
Funder
Directorate for Engineering
Publisher
AIP Publishing
Subject
Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering
Link
http://aip.scitation.org/doi/pdf/10.1063/1.5056540
Reference47 articles.
1. Advanced injection and mixing techniques for scramjet combustors
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5. Compressibility effects in a turbulent annular mixing layer. Part 2. Mixing of a passive scalar
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