An experimental investigation of the flow dynamics of streamwise vortices of various strengths interacting with a supersonic jet
Author:
Affiliation:
1. Department of Aerospace Engineering & Engineering Mechanics, University of Cincinnati, Cincinnati, Ohio 45220, USA
2. Naval Research Laboratory, Washington, D.C. 20375, USA
Funder
Office of Naval Research (ONR)
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/10.1063/1.4892008
Reference36 articles.
1. Control of an axisymmetric jet using vortex generators
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4. Effects of the initial condition on the axisymmetric free shear layer: Effect of the initial fluctuation level
5. Noise reduction in supersonic jets by nozzle fluidic inserts
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