Large-eddy simulation of a spatially-evolving supersonic turbulent boundary layer at \(M_{\infty} = 2\)
DOI10.1016/j.euromechflu.2017.09.005zbMath1408.76328OpenAlexW2757580286MaRDI QIDQ1672430
O. Ben-Nasr, Arnab Chaudhuri, Abdellah Hadjadj, Mostafa Safdari Shadloo
Publication date: 10 September 2018
Published in: European Journal of Mechanics. B. Fluids (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/j.euromechflu.2017.09.005
coherent structures model (CSM)dynamic Smagorinsky model (DSM)subgrid-scale (SGS) modelingsupersonic turbulent boundary layer (STBL)wall-adapting local eddy-viscosity (WALE)implicit LES (ILES)
Shear flows and turbulence (76F10) Direct numerical and large eddy simulation of turbulence (76F65) Supersonic flows (76J20)
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Cites Work
- Unnamed Item
- Statistical characteristics of an isothermal, supersonic developing boundary layer flow from DNS data
- Large-eddy simulation of turbulent channel flows with conservative IDO scheme
- Invariant analysis of turbulent pipe flow.
- Assessment of subgrid-scale modeling for large-eddy simulation of a spatially-evolving compressible turbulent boundary layer
- A digital filter based generation of inflow data for spatially developing direct numerical or large eddy simulations.
- Subgrid-scale stress modelling based on the square of the velocity gradient tensor
- Generalized conservative approximations of split convective derivative operators
- Turbulent supersonic channel flow
- Turbulence in supersonic boundary layers at moderate Reynolds number
- Direct numerical simulation of hypersonic turbulent boundary layers. Part 2. Effect of wall temperature
- Direct numerical simulation and analysis of a spatially evolving supersonic turbulent boundary layer at M=2.25
- Statistical theory for compressible turbulent shear flows, with the application to subgrid modeling
- Computational Modeling of Turbulent Flows
- A dynamic subgrid-scale model for compressible turbulence and scalar transport
- Direct numerical simulation of a supersonic turbulent boundary layer at Mach 2.5
- Turbulent Flows
- Direct numerical simulation of compressible turbulent channel flow between adiabatic and isothermal walls
- Compressible turbulent channel flows: DNS results and modelling
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