Add to ORKGWe consider the solution of the steady state compressible Navier-Stokes equations for both stationary and rotating turbo-machinery. This is augmented by a k ε turbulence model. The body boundary is modeled using wall functions which allows th
This paper presents a numerical method for the simulation of flow in turbomachinery blade rows using...
Efficient preconditioned multigrid methods are developed for both inviscid and viscous flow applicat...
Efficient preconditioned multigrid methods are developed for both inviscid and viscous flow applicat...
The MSU TURBO code, distributed to U.S. engine companies by NASA Glenn, is a heavily used parallel c...
An improved preconditioning is proposed for viscous flow computations in rotating and nonrotating fr...
A preconditioned solution scheme for the computation of compressible flow in turbomachinery at arbit...
An implicit procedure based on the artificial compressibility formulation is presented for the numer...
An implicit procedure based on the artificial compressibility formulation is presented for the numer...
A computer code has been developed to predict three-dimensional incompressible turbulent flow in com...
The linear harmonic approach has been applied for solving problems involving for example blade vibra...
The adequate representation of turbulence is crucial for the predictive accuracy of the computationa...
The simulation quality of numerical flow simulations depends on the choice of physical modelling as ...
We consider the steady-state equations for a compressible fluid. For low-speed flow, the system is s...
The flow in a multistage turbomachinery blade row is compressible, viscous, and unsteady. Complex fl...
A preconditioning scheme has been implemented into a three-dimensional viscous computational fluid d...
This paper presents a numerical method for the simulation of flow in turbomachinery blade rows using...
Efficient preconditioned multigrid methods are developed for both inviscid and viscous flow applicat...
Efficient preconditioned multigrid methods are developed for both inviscid and viscous flow applicat...
The MSU TURBO code, distributed to U.S. engine companies by NASA Glenn, is a heavily used parallel c...
An improved preconditioning is proposed for viscous flow computations in rotating and nonrotating fr...
A preconditioned solution scheme for the computation of compressible flow in turbomachinery at arbit...
An implicit procedure based on the artificial compressibility formulation is presented for the numer...
An implicit procedure based on the artificial compressibility formulation is presented for the numer...
A computer code has been developed to predict three-dimensional incompressible turbulent flow in com...
The linear harmonic approach has been applied for solving problems involving for example blade vibra...
The adequate representation of turbulence is crucial for the predictive accuracy of the computationa...
The simulation quality of numerical flow simulations depends on the choice of physical modelling as ...
We consider the steady-state equations for a compressible fluid. For low-speed flow, the system is s...
The flow in a multistage turbomachinery blade row is compressible, viscous, and unsteady. Complex fl...
A preconditioning scheme has been implemented into a three-dimensional viscous computational fluid d...
This paper presents a numerical method for the simulation of flow in turbomachinery blade rows using...
Efficient preconditioned multigrid methods are developed for both inviscid and viscous flow applicat...
Efficient preconditioned multigrid methods are developed for both inviscid and viscous flow applicat...