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Direct numerical simulations of supersonic turbulent shear layers show that the asymmetric behavior and entrainment ratio increase with compressibility and velocity difference, a key insight for designing advanced supersonic combustors.
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This page is a summary of: Entrainment and Asymmetry in Spatially Developing Supersonic Turbulent Shear Layers, July 2024, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/6.2024-3885.
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