A revised version of a split-velocity method for numerical calculation of compressible duct flow was developed. The revision incorporates balancing of mass flow rates on each marching step in order to maintain front-to-back continuity during the calculation. The (checkerboard) zebra algorithm is applied to solution of the three-dimensional continuity equation in conservative form. A second-order A-stable linear multistep method is employed in effecting a marching solution of the parabolized momentum equations. A checkerboard successive overrelaxation iteration is used to solve the resulting implicit nonlinear systems of finite-difference equations which govern stepwise transition
The research program for the first year of this project (see the original research proposal) consist...
A numerical solution algorithm is established for prediction of subsonic turbulent three-dimensional...
Efficient iterative solution methods are being developed for the numerical solution of two- and thre...
A revised version of Dodge's split-velocity method for numerical calculation of compressible duct fl...
Downstream marching iterative schemes for the solution of the Parabolized or Thin Layer (PNS or TL) ...
A noniterative, implicit, space-marching, finite-difference algorithm was developed for the steady t...
A new computer code for the solution of the three-dimensional parabolized Navier-Stokes (PNS) equati...
An implicit, space-marching, finite-difference procedure is presented for solving the primitive vari...
A three-dimensional parabolic Navier-Stokes code, PEPSIG, was used to analyze the flow in the subson...
An accurate and efficient numerical solution algorithm is established for solution of the high Reyno...
A three dimensional analysis for fully viscous, subsonic, compressible flow is evaluated. An approxi...
An explicit, upwind algorithm was developed for the direct (noniterative) integration of the 3-D Par...
A Navier-Stokes equations solver based on a pressure correction method with a pressure-staggered mes...
A new numerical method which was used to reduce the computation time required in fluid dynamics to s...
The three-dimensional compressible Navier-Stokes equations are formulated in a rotating coordinate s...
The research program for the first year of this project (see the original research proposal) consist...
A numerical solution algorithm is established for prediction of subsonic turbulent three-dimensional...
Efficient iterative solution methods are being developed for the numerical solution of two- and thre...
A revised version of Dodge's split-velocity method for numerical calculation of compressible duct fl...
Downstream marching iterative schemes for the solution of the Parabolized or Thin Layer (PNS or TL) ...
A noniterative, implicit, space-marching, finite-difference algorithm was developed for the steady t...
A new computer code for the solution of the three-dimensional parabolized Navier-Stokes (PNS) equati...
An implicit, space-marching, finite-difference procedure is presented for solving the primitive vari...
A three-dimensional parabolic Navier-Stokes code, PEPSIG, was used to analyze the flow in the subson...
An accurate and efficient numerical solution algorithm is established for solution of the high Reyno...
A three dimensional analysis for fully viscous, subsonic, compressible flow is evaluated. An approxi...
An explicit, upwind algorithm was developed for the direct (noniterative) integration of the 3-D Par...
A Navier-Stokes equations solver based on a pressure correction method with a pressure-staggered mes...
A new numerical method which was used to reduce the computation time required in fluid dynamics to s...
The three-dimensional compressible Navier-Stokes equations are formulated in a rotating coordinate s...
The research program for the first year of this project (see the original research proposal) consist...
A numerical solution algorithm is established for prediction of subsonic turbulent three-dimensional...
Efficient iterative solution methods are being developed for the numerical solution of two- and thre...