The numerical solution of the Navier-Stokes equations about three-dimensional configurations is reviewed. Formulational and computational requirements for the various Navier-Stokes approaches are examined for typical problems including the viscous flow field solution about a complete aerospace vehicle. Recent computed results, with experimental comparisons when available, are presented to highlight the presentation. The future of Navier-Stokes applications in three-dimensions is seen to be rapidly expanding across a broad front including internal and external flows, and flows across the entire speed regime from incompressible to hypersonic applications. Prospects for the future are described and recommendations for areas of concentrated res...
Transonic flow fields about wing geometries are computed using an Euler/Navier-Stokes approach in wh...
An overview of the computational requirements for the13; application of Navier-Stokes equations in t...
The accurate calculation of three-dimensional internal flowfields for application towards aerospace ...
Critical to the advancement of computational aerodynamics capability is the ability to simulate flow...
A computational fluid dynamics tool has been developed capable of analyzing the viscous supersonic/h...
A computer analysis was developed for calculating steady (or unsteady) three-dimensional aircraft co...
The performance of a three-dimensional Navier-Stokes solution technique in predicting the transonic ...
The Navier-Stokes equations are solved numerically. These equations are unsteady, compressible, visc...
The overall objective of the research carried out over the last two years was the development of new...
An explicit multistage Runge-Kutta type of time-stepping scheme is used for solving transonic flow p...
The objective of research was to develop and validate new computational algorithms for solving the s...
Several incompressible Navier-Stokes solution methods for obtaining steady and unsteady solutions ar...
An unfactored implicit time-marching method for the solution of the three dimensional Navier-Stokes...
A numerical method is presented to solve the three-dimensional Navier-Stokes equations in combinatio...
The past decade has seen considerable activity in algorithm development for the Navier-Stokes equati...
Transonic flow fields about wing geometries are computed using an Euler/Navier-Stokes approach in wh...
An overview of the computational requirements for the13; application of Navier-Stokes equations in t...
The accurate calculation of three-dimensional internal flowfields for application towards aerospace ...
Critical to the advancement of computational aerodynamics capability is the ability to simulate flow...
A computational fluid dynamics tool has been developed capable of analyzing the viscous supersonic/h...
A computer analysis was developed for calculating steady (or unsteady) three-dimensional aircraft co...
The performance of a three-dimensional Navier-Stokes solution technique in predicting the transonic ...
The Navier-Stokes equations are solved numerically. These equations are unsteady, compressible, visc...
The overall objective of the research carried out over the last two years was the development of new...
An explicit multistage Runge-Kutta type of time-stepping scheme is used for solving transonic flow p...
The objective of research was to develop and validate new computational algorithms for solving the s...
Several incompressible Navier-Stokes solution methods for obtaining steady and unsteady solutions ar...
An unfactored implicit time-marching method for the solution of the three dimensional Navier-Stokes...
A numerical method is presented to solve the three-dimensional Navier-Stokes equations in combinatio...
The past decade has seen considerable activity in algorithm development for the Navier-Stokes equati...
Transonic flow fields about wing geometries are computed using an Euler/Navier-Stokes approach in wh...
An overview of the computational requirements for the13; application of Navier-Stokes equations in t...
The accurate calculation of three-dimensional internal flowfields for application towards aerospace ...