A study of inviscid, supersonic mixing layers using a second-order total variational diminishing scheme
Author:
Affiliation:
1. University of Washington, Seattle, Washington
2. University of Utah, Salt Lake City, Utah
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.10333
Reference19 articles.
1. On density effects and large structure in turbulent mixing layers
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3. The mixing layer: deterministic models of a turbulent flow. Part 1. Introduction and the two-dimensional flow
4. Direct Numerical Simulation of a Perturbed, Turbulent Mixing Layer
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1. Numerical simulation of nonlinear interactions of supersonic instability modes in a high-speed mixing layer;HIGH-ENERGY PROCESSES IN CONDENSED MATTER (HEPCM 2020): Proceedings of the XXVII Conference on High-Energy Processes in Condensed Matter, dedicated to the 90th anniversary of the birth of RI Soloukhin;2020
2. Planar velocity measurements in compressible mixing layers;Journal of Fluid Mechanics;2001-03-25
3. ADM‐WENO scheme and its application in compressible mixing flows;International Journal of Numerical Methods for Heat & Fluid Flow;1999-06-01
4. Numerical Simulation of Nonlinear Interactions in Subsonic and Supersonic Free Shear Layers;IUTAM Symposium on Dynamics of Slender Vortices;1998
5. Computational study of the inviscid, nonlinear physics of supersonic base flows;33rd Aerospace Sciences Meeting and Exhibit;1995-01-09
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