This paper presents the formulation of a dual time stepping procedure to solve the equations of fully implicit Runge-Kutta schemes. In particular the method is applied to Gauss and Radau 2A schemes with either two or three stages. The schemes are tested for unsteady flows over a pitching airfoil modeled by both the Euler and the unsteady Reynolds averaged Navier Stokes (URANS) equations. It is concluded that the Radau 2A schemes are more robust and less computationally expensive because they require a much smaller number of inner iterations. Moreover these schemes seem to be competitive with alternative implicit schemes. I
Implicit time integration was studied in the context of unsteady shock-boundary layer interaction fl...
Efcient time integration is of the utmost concern for unsteady ow computations. Within this context ...
Runge-Kutta/Implicit methods for the solution of the Navier-Stokes equations provide superior conver...
Based on an existing code for the solution of two-dimensional unsteady Navier-Stokes equations using...
The prediction of unsteady air-loads on airfoils and wings plays an increasing role in the aircraft ...
A dual time-stepping algorithm has been developed for the efficient computation of unsteady fluid dy...
In this study we generate optimal Runge-Kutta (RK) schemes for converging the Artificial Compressibi...
Efficient time integration is of the utmost concern for unsteady flow computations. Within this cont...
A three-stage Runge-Kutta (RK) scheme with multigrid and an implicit preconditioner has been shown t...
Unsteady computational fluid dynamics (CFD) is increasingly becoming a critical tool in the developm...
This paper reports development of an unstructured high-order compact method for solving two-dimensio...
The convergence of a Runge-Kutta (RK) scheme with multigrid is accelerated by preconditioning with a...
In this paper, two semi-implicit Runge-Kutta algorithms are developed for the simula-tion of wall-bo...
A novel time integration approach is explored for unsteady flow computations. It is a multi-block fo...
The numerical behavior of two implicit time-marching methods is investigated in solving two-dimensio...
Implicit time integration was studied in the context of unsteady shock-boundary layer interaction fl...
Efcient time integration is of the utmost concern for unsteady ow computations. Within this context ...
Runge-Kutta/Implicit methods for the solution of the Navier-Stokes equations provide superior conver...
Based on an existing code for the solution of two-dimensional unsteady Navier-Stokes equations using...
The prediction of unsteady air-loads on airfoils and wings plays an increasing role in the aircraft ...
A dual time-stepping algorithm has been developed for the efficient computation of unsteady fluid dy...
In this study we generate optimal Runge-Kutta (RK) schemes for converging the Artificial Compressibi...
Efficient time integration is of the utmost concern for unsteady flow computations. Within this cont...
A three-stage Runge-Kutta (RK) scheme with multigrid and an implicit preconditioner has been shown t...
Unsteady computational fluid dynamics (CFD) is increasingly becoming a critical tool in the developm...
This paper reports development of an unstructured high-order compact method for solving two-dimensio...
The convergence of a Runge-Kutta (RK) scheme with multigrid is accelerated by preconditioning with a...
In this paper, two semi-implicit Runge-Kutta algorithms are developed for the simula-tion of wall-bo...
A novel time integration approach is explored for unsteady flow computations. It is a multi-block fo...
The numerical behavior of two implicit time-marching methods is investigated in solving two-dimensio...
Implicit time integration was studied in the context of unsteady shock-boundary layer interaction fl...
Efcient time integration is of the utmost concern for unsteady ow computations. Within this context ...
Runge-Kutta/Implicit methods for the solution of the Navier-Stokes equations provide superior conver...