Large-eddy Simulation of Supersonic Boundary-layer Flow by a High-order Method
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Publication:4651389
DOI10.1080/10618560310001614926zbMath1063.76609OpenAlexW2007574366MaRDI QIDQ4651389
Miguel R. Visbal, Donald P. Rizzetta
Publication date: 21 February 2005
Published in: International Journal of Computational Fluid Dynamics (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1080/10618560310001614926
Finite difference methods applied to problems in fluid mechanics (76M20) Supersonic flows (76J20) Boundary-layer theory for compressible fluids and gas dynamics (76N20)
Related Items (4)
Resolution effects in compressible, turbulent boundary layer simulations ⋮ Implicit eighth-order central compact scheme for the numerical simulation of steady and unsteady incompressible Navier–Stokes equations ⋮ Delay of finite-span excrescence-induced transition using plasma-based control ⋮ Implicit large eddy simulation of a supersonic flat-plate boundary layer flow by weighted compact nonlinear scheme
Uses Software
Cites Work
- A diagonal form of an implicit approximate-factorization algorithm
- Compact finite difference schemes with spectral-like resolution
- Large-eddy simulation of the shock/turbulence interaction
- Statistical theory for compressible turbulent shear flows, with the application to subgrid modeling
- A dynamic subgrid-scale model for compressible turbulence and scalar transport
- An Implicit Factored Scheme for the Compressible Navier-Stokes Equations
- Numerical simulation of delta-wing roll
- Direct numerical simulation of a supersonic turbulent boundary layer at Mach 2.5
- Direct numerical simulation of controlled transition in a flat-plate boundary layer
- Large Eddy Simulation of Flow Transition in a Compressible Flat-Plate Boundary Layer at Mach 4.5
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