Dynamic hybridization of MILES and RANS for predicting airfoil stall

DOI10.1016/J.COMPFLUID.2007.06.004zbMath1194.76084OpenAlexW2045346603MaRDI QIDQ993961

Toshiaki Ikohagi, Ichiro Nakamori

Publication date: 16 September 2010

Published in: Computers and Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.compfluid.2007.06.004

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) Direct numerical and large eddy simulation of turbulence (76F65) Compressibility effects in turbulence (76F50)

Uses Software

• Spalart-Allmaras

Cites Work

• Computation of turbulent supersonic flows around pointed bodies having crossflow separation
• Approximate Riemann solvers, parameter vectors, and difference schemes
• An approach to wall modeling in large-eddy simulations
• Numerical investigations of flow over a sphere in the subcritical and supercritical regimes
• Computational Aerodynamics Development and Outlook
• A dynamic subgrid-scale eddy viscosity model
• Developing high-order weighted compact nonlinear schemes

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