International audienceThis paper applies a recently developed immersed boundary-turbulence wall modeling approach to turbulent flows over a generic car geometry, known as the Ahmed body, under massive flow separation within a lattice Boltzmann solver. Although the immersed boundary method combined with hierarchical Cartesian grid offers high flexibility in automatic grid generation around complex geometries, the near-wall solution is significantly deteriorated compared to the body-fitted simulation, especially when coupled to wall models for turbulent flows at high Reynolds number. Enhanced wall treatments have been proposed in the literature and validated for attached flow configurations. In this work, the Ahmed body with a slant surface o...
Turbulent flows present structures with a wide range of scales. The computation of the complete phys...
Research is presented on the development and testing of a new procedure for the time dependent, spat...
The aerodynamics of aircraft high-lift devices at near-stall conditions is particularly difficult to...
International audienceAn immersed boundary method is coupled to a turbulent wall model and Large Edd...
International audienceThe article deals with an improved treatment of wall models for the simulation...
Delayed detached eddy simulation based on the Spalart–Allmaras turbulence model is applied in conjun...
International audienceAn improved coupling of immersed boundary method and turbulence wall models on...
Approximate immersed boundary conditions for large-eddy simulation (LES) of turbulent flows in combi...
The aim of this work is to propose a new wall model for separated flows which is combined with large...
Immersed boundary methods are frequently employed for simulating flows at low Reynolds numbers or fo...
International audiencePurpose: The Lattice Boltzmann (LB) method offers an alternative to convention...
A non-equilibrium wall model for large-eddy simulation with the immersed boundary (IB) method is pro...
An efficient and accurate finite volume incompressible flow solver with a staggered arrangement in t...
A novel method is proposed to combine the wall-modeled large-eddy simulation (LES) with the diffuse-...
The Ahmed body is one of the most well-investigated vehicle bodies for aerodynamic purposes. Despite...
Turbulent flows present structures with a wide range of scales. The computation of the complete phys...
Research is presented on the development and testing of a new procedure for the time dependent, spat...
The aerodynamics of aircraft high-lift devices at near-stall conditions is particularly difficult to...
International audienceAn immersed boundary method is coupled to a turbulent wall model and Large Edd...
International audienceThe article deals with an improved treatment of wall models for the simulation...
Delayed detached eddy simulation based on the Spalart–Allmaras turbulence model is applied in conjun...
International audienceAn improved coupling of immersed boundary method and turbulence wall models on...
Approximate immersed boundary conditions for large-eddy simulation (LES) of turbulent flows in combi...
The aim of this work is to propose a new wall model for separated flows which is combined with large...
Immersed boundary methods are frequently employed for simulating flows at low Reynolds numbers or fo...
International audiencePurpose: The Lattice Boltzmann (LB) method offers an alternative to convention...
A non-equilibrium wall model for large-eddy simulation with the immersed boundary (IB) method is pro...
An efficient and accurate finite volume incompressible flow solver with a staggered arrangement in t...
A novel method is proposed to combine the wall-modeled large-eddy simulation (LES) with the diffuse-...
The Ahmed body is one of the most well-investigated vehicle bodies for aerodynamic purposes. Despite...
Turbulent flows present structures with a wide range of scales. The computation of the complete phys...
Research is presented on the development and testing of a new procedure for the time dependent, spat...
The aerodynamics of aircraft high-lift devices at near-stall conditions is particularly difficult to...