A numerical method is presented for solving the parabolic-elliptic Navier-Stokes equations. The solution procedure is applied to three-dimensional supersonic laminar jet flow issuing parallel with a supersonic free stream. A coordinate transformation is introduced which maps the boundaries at infinity into a finite computational domain in order to eliminate difficulties associated with the imposition of free-stream boundary conditions. Results are presented for an approximate circular jet, a square jet, varying aspect ratio rectangular jets, and interacting square jets. The solution behavior varies from axisymmetric to nearly two-dimensional in character. For cases where comparisons of the present results with those obtained from shear laye...
The research program for the first year of this project (see the original research proposal) consist...
A computer implemented numerical method for predicting the flow in and about an isolated three dimen...
Three-dimensional, incompressible turbulent jets with rectangular and elliptical cross-section are s...
A numerical method is presented which is valid for integration of the parabolic-elliptic Navier-Stok...
The proper use of a computational fluid dynamics code requires a good understanding of the particula...
An explicit, upwind algorithm was developed for the direct (noniterative) integration of the 3-D Par...
This report presents a unified method for subsonic and supersonic jet analysis using the three-dimen...
Finite difference methods were applied to solve the parabolic Navier-Stokes equations for the flow o...
Flows of relevance to new generation aerospace vehicles exist, which are weakly dependent on the str...
The Navier-Stokes equations are solved numerically. These equations are unsteady, compressible, visc...
A noniterative, implicit, space-marching, finite-difference algorithm was developed for the steady t...
A numerical solution algorithm is established for prediction of subsonic turbulent three-dimensional...
A new computer code for the solution of the three-dimensional parabolized Navier-Stokes (PNS) equati...
Flows of relevance to new generation aerospace vehicles exist, which are weakly de-pendent on the st...
Systematic numerical analysis of two dimensional and axisymmetric laminar jet of incompressible flui...
The research program for the first year of this project (see the original research proposal) consist...
A computer implemented numerical method for predicting the flow in and about an isolated three dimen...
Three-dimensional, incompressible turbulent jets with rectangular and elliptical cross-section are s...
A numerical method is presented which is valid for integration of the parabolic-elliptic Navier-Stok...
The proper use of a computational fluid dynamics code requires a good understanding of the particula...
An explicit, upwind algorithm was developed for the direct (noniterative) integration of the 3-D Par...
This report presents a unified method for subsonic and supersonic jet analysis using the three-dimen...
Finite difference methods were applied to solve the parabolic Navier-Stokes equations for the flow o...
Flows of relevance to new generation aerospace vehicles exist, which are weakly dependent on the str...
The Navier-Stokes equations are solved numerically. These equations are unsteady, compressible, visc...
A noniterative, implicit, space-marching, finite-difference algorithm was developed for the steady t...
A numerical solution algorithm is established for prediction of subsonic turbulent three-dimensional...
A new computer code for the solution of the three-dimensional parabolized Navier-Stokes (PNS) equati...
Flows of relevance to new generation aerospace vehicles exist, which are weakly de-pendent on the st...
Systematic numerical analysis of two dimensional and axisymmetric laminar jet of incompressible flui...
The research program for the first year of this project (see the original research proposal) consist...
A computer implemented numerical method for predicting the flow in and about an isolated three dimen...
Three-dimensional, incompressible turbulent jets with rectangular and elliptical cross-section are s...