Unstructured grid simulations of spatially evolving supersonic shear layers
Author:
Affiliation:
1. University of Illinois at Urbana-Champaign, Urbana, Illinois 61801
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.12675
Reference37 articles.
1. Structure of Turbulent Shear Flows: A New Look
2. Vortex pairing : the mechanism of turbulent mixing-layer growth at moderate Reynolds number
3. Two-dimensional shear-layer entrainment
4. The effect of initial conditions on the development of a free shear layer
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1. Sensitivity analysis of initial condition parameters on the transitional temporal turbulent mixing layer;Journal of Turbulence;2008-01
2. Large-scale structure visualization and convection velocity in supersonic blunt-base cylinder wakes;Physics of Fluids;2007-01
3. A compressible Navier–Stokes flow solver with scalar transport;Journal of Computational Physics;2005-04
4. Time-Correlated Visualizations of Supersonic Blunt-Base Cylinder Wakes;43rd AIAA Aerospace Sciences Meeting and Exhibit;2005-01-10
5. Streamwise Vortex Structure Induced by Secondary Instability of Compressible Shear Flow;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2005
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