February 1981Includes bibliographical references (page 58)An implicit factored algorithm for the solution of the thin shear layer approximation of the Navier-Stokes equations is described and explicit boundary conditions are developed for internal flow problems. This scheme is compared to theoretical predictions and experimental data, as well as to other more thoroughly tested numerical schemes. The examples presented demonstrate the ability of the factored algorithm to accurately predict internal flow fields and provide insight into the difficulties associated with the numerical simulation of internal flow fields.NASA Lewis Research Center Grant no. NAG3-
A noniterative, implicit, space-marching, finite-difference algorithm was developed for the steady t...
A computer analysis was developed for calculating steady (or unsteady) three-dimensional aircraft co...
Five viscous transonic airfoil cases were computed by two significantly different computational flui...
An implicit analogue of a widely used explicit method to external axisymmetric laminar flows with st...
Thin-Layer Navier-Stokes equations in generalized body-fitted coordinate system and non-dimensional ...
Inlet flow fields for airbreathing missiles are calculated by the adaptation of a two dimensional co...
The Navier-Stokes equations are solved numerically for two-dimensional steady viscous laminar flows....
The Navier-Stokes equations are solved numerically for two-dimensional steady viscous laminar flows....
grantor: University of TorontoA time-accurate, implicit numerical method for the two-dimen...
grantor: University of TorontoA time-accurate, implicit numerical method for the two-dimen...
Numerical procedures for solving the thin-shear-layer Navier-Stokes equations and for the interactio...
Inlet flow fields are calculated by an implicit, time marching procedure to solve the thin layer Nav...
A finite-volume scheme for numerical integration of the Euler equations was extended to allow soluti...
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 ...
A noniterative, implicit, space-marching, finite-difference algorithm was developed for the steady t...
A computer analysis was developed for calculating steady (or unsteady) three-dimensional aircraft co...
Five viscous transonic airfoil cases were computed by two significantly different computational flui...
An implicit analogue of a widely used explicit method to external axisymmetric laminar flows with st...
Thin-Layer Navier-Stokes equations in generalized body-fitted coordinate system and non-dimensional ...
Inlet flow fields for airbreathing missiles are calculated by the adaptation of a two dimensional co...
The Navier-Stokes equations are solved numerically for two-dimensional steady viscous laminar flows....
The Navier-Stokes equations are solved numerically for two-dimensional steady viscous laminar flows....
grantor: University of TorontoA time-accurate, implicit numerical method for the two-dimen...
grantor: University of TorontoA time-accurate, implicit numerical method for the two-dimen...
Numerical procedures for solving the thin-shear-layer Navier-Stokes equations and for the interactio...
Inlet flow fields are calculated by an implicit, time marching procedure to solve the thin layer Nav...
A finite-volume scheme for numerical integration of the Euler equations was extended to allow soluti...
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 ...
A noniterative, implicit, space-marching, finite-difference algorithm was developed for the steady t...
A computer analysis was developed for calculating steady (or unsteady) three-dimensional aircraft co...
Five viscous transonic airfoil cases were computed by two significantly different computational flui...