Direct simulation of a Mach-5 turbulent spatially-developing boundary layer
Author:
Affiliation:
1. University of Puerto Rico
2. University of Colorado, Boulder
Publisher
American Institute of Aeronautics and Astronautics
Reference24 articles.
1. A dynamic multi-scale approach for turbulent inflow boundary conditions in spatially developing flows
2. DNS of a Large-Domain, Mach 3 Turbulent Boundary Layer: Turbulence Structure
3. Direct numerical simulation of hypersonic turbulent boundary layers. Part 2. Effect of wall temperature
4. Direct numerical simulation of hypersonic turbulent boundary layers. Part 3. Effect of Mach number
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1. Investigation of Unconventional Coherent Structures in Implicit Large Eddy Simulations of Supersonic Turbulent Boundary Layers;AIAA SCITECH 2024 Forum;2024-01-04
2. Evaluating the Impact of Lossy Compression on a Direct Numerical Simulation of a Mach 2.5 Turbulent Boundary Layer;AIAA SCITECH 2023 Forum;2023-01-19
3. Wall pressure fluctuations in supersonic boundary layers over compression ramps with different turning angles;Physics of Fluids;2022-12
4. Compressibility and Reynolds number effect on Lagrangian Coherent Structures (LCS);AIAA AVIATION 2022 Forum;2022-06-20
5. Power spectrum analysis in supersonic/hypersonic turbulent boundary layers;AIAA SCITECH 2022 Forum;2022-01-03
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