Add to ORKGThe fluid flow inside the space shuttle main engine (SSME) traverses through a complex geometrical configuration. The flow is compressible, viscous, and turbulent with pockets of separated regions. Several computer codes are being developed to solve three dimensional Navier-Stokes equations with different turbulence models for analyzing the SSME internal flow. The locally implicit scheme is a computationally efficient scheme which converges rapidly in multi-grid modes for elliptic problems. It has the promise of providing a rapidly converging algorithm for steady-state viscous flow problems
Several incompressible Navier-Stokes solution methods for obtaining steady and unsteady solutions ar...
The objective of research was to develop and validate new computational algorithms for solving the s...
Implicit finite difference schemes are often the preferred numerical schemes in computational fluid ...
Computation of the flow field inside a space shuttle main engine (SSME) requires the application of ...
The Navier-Stokes equations are solved numerically for two-dimensional steady viscous laminar flows....
A noniterative, implicit, space-marching, finite-difference algorithm was developed for the steady t...
A single level effectively explicit implicit algorithm for gasdynamics is presented. The method meet...
Efficient acceleration techniques typical of explicit steady-state solvers are extended to time-accu...
Implicit methods were developed and tested for unstructured mesh computations. The approximate syste...
For a computational flow simulation tool to be useful in a design environment, it must be very robus...
An upwind MUSCL type implicit scheme for the three-dimensional Navier-Stokes equations is presented....
The compressible Euler and Navier-Stokes equations represent the most sophisticatedmodels of single-...
An explicit-implicit technique for solving Navier-Stokes equations is described which, is much less ...
Aims. We describe and study a family of new multigrid iterative solvers for the multidimensional, im...
grantor: University of TorontoA time-accurate, implicit numerical method for the two-dimen...
Several incompressible Navier-Stokes solution methods for obtaining steady and unsteady solutions ar...
The objective of research was to develop and validate new computational algorithms for solving the s...
Implicit finite difference schemes are often the preferred numerical schemes in computational fluid ...
Computation of the flow field inside a space shuttle main engine (SSME) requires the application of ...
The Navier-Stokes equations are solved numerically for two-dimensional steady viscous laminar flows....
A noniterative, implicit, space-marching, finite-difference algorithm was developed for the steady t...
A single level effectively explicit implicit algorithm for gasdynamics is presented. The method meet...
Efficient acceleration techniques typical of explicit steady-state solvers are extended to time-accu...
Implicit methods were developed and tested for unstructured mesh computations. The approximate syste...
For a computational flow simulation tool to be useful in a design environment, it must be very robus...
An upwind MUSCL type implicit scheme for the three-dimensional Navier-Stokes equations is presented....
The compressible Euler and Navier-Stokes equations represent the most sophisticatedmodels of single-...
An explicit-implicit technique for solving Navier-Stokes equations is described which, is much less ...
Aims. We describe and study a family of new multigrid iterative solvers for the multidimensional, im...
grantor: University of TorontoA time-accurate, implicit numerical method for the two-dimen...
Several incompressible Navier-Stokes solution methods for obtaining steady and unsteady solutions ar...
The objective of research was to develop and validate new computational algorithms for solving the s...
Implicit finite difference schemes are often the preferred numerical schemes in computational fluid ...