Impact of tab location relative to the nozzle exit on the shock structure of a supersonic jet
Author:
Affiliation:
1. Mechanical Engineering, Indian Institute of Technology Jammu, Jammu 181221, India
2. Aerospace Engineering, Indian Institute of Technology Kanpur, Kanpur 208016, India
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/10.1063/1.5111328
Reference45 articles.
1. FLOW CONTROL WITH NONCIRCULAR JETS
2. On density effects and large structure in turbulent mixing layers
3. Structure of Turbulent Shear Flows: A New Look
4. The distortion of a jet by tabs
5. Three-dimensional evolution of flow structures in transitional circular and chevron jets
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