Add to ORKGA computational fluid dynamics tool has been developed capable of analyzing the viscous supersonic/hypersonic flow about realistic configurations. This techniques can predict the flow in regions of canopies, wings, and canards in addition to the usual simple symmetric configurations. It also allows for interactions between aerodynamic surfaces such as the vortex interaction between canards and wings
A computer analysis was developed for calculating steady (or unsteady) three-dimensional aircraft co...
Computations of three dimensional vortical flows over a generic High Speed Civil Transport (HSCT) co...
A multigrid acceleration technique developed for solving 3-D Navier-Stokes equations for subsonic/tr...
The numerical solution of the Navier-Stokes equations about three-dimensional configurations is revi...
Research in aerodynamics is discussed. The development of equilibrium air curve fits; computation of...
A procedure is presented, as well as some results, to calculate the flow over a generic fighter conf...
Critical to the advancement of computational aerodynamics capability is the ability to simulate flow...
The present paper describes a numerical mesh generation technique to be used with an implicit finite...
A Navier-Stokes computer code was validated using a number of two- and three-dimensional configurati...
While the zonal grid system of Transonic Navier-Stokes (TNS) provides excellent modeling of complex ...
The accurate calculation of three-dimensional internal flowfields for application towards aerospace ...
The Reynolds averaged Navier-Stokes equations are solved numerically for a variety of transonic airf...
A numerical procedure was developed to compute the inviscid super/hypersonic flow fields about compl...
The performance of a three-dimensional Navier-Stokes solution technique in predicting the transonic ...
A numerical solution algorithm is established for prediction of subsonic turbulent three-dimensional...
A computer analysis was developed for calculating steady (or unsteady) three-dimensional aircraft co...
Computations of three dimensional vortical flows over a generic High Speed Civil Transport (HSCT) co...
A multigrid acceleration technique developed for solving 3-D Navier-Stokes equations for subsonic/tr...
The numerical solution of the Navier-Stokes equations about three-dimensional configurations is revi...
Research in aerodynamics is discussed. The development of equilibrium air curve fits; computation of...
A procedure is presented, as well as some results, to calculate the flow over a generic fighter conf...
Critical to the advancement of computational aerodynamics capability is the ability to simulate flow...
The present paper describes a numerical mesh generation technique to be used with an implicit finite...
A Navier-Stokes computer code was validated using a number of two- and three-dimensional configurati...
While the zonal grid system of Transonic Navier-Stokes (TNS) provides excellent modeling of complex ...
The accurate calculation of three-dimensional internal flowfields for application towards aerospace ...
The Reynolds averaged Navier-Stokes equations are solved numerically for a variety of transonic airf...
A numerical procedure was developed to compute the inviscid super/hypersonic flow fields about compl...
The performance of a three-dimensional Navier-Stokes solution technique in predicting the transonic ...
A numerical solution algorithm is established for prediction of subsonic turbulent three-dimensional...
A computer analysis was developed for calculating steady (or unsteady) three-dimensional aircraft co...
Computations of three dimensional vortical flows over a generic High Speed Civil Transport (HSCT) co...
A multigrid acceleration technique developed for solving 3-D Navier-Stokes equations for subsonic/tr...