The problem of obtaining three dimensional grids with sufficient resolution to resolve all the flow or other physical features of interest is addressed. The generation of a computational grid involves a series of compromises to resolve several conflicting requirements. On one hand, one would like the grid to be fine enough and not too skewed to reduce the numerical errors and to adequately resolve the pertinent physical features of the flow field about the aircraft. On the other hand, the capabilities of present or even future supercomputers are finite and the number of mesh points must be limited to a reasonable number: one which is usually much less than desired for numerical accuracy. One technique to overcome this limitation is the 'zon...
The thin-layer Navier-Stokes equations are coupled with a zonal scheme (or domain-decomposition meth...
Important issues involved in working with complex geometries are discussed. Approaches taken to addr...
Grid generation and Euler flow about fighter aircraft are described. A fighter aircraft geometry is ...
The computation of flow over complex geometries, such as realistic aircraft configurations, poses di...
A suitable grid system for complex three dimensional configurations such as wing/body/nacelle shape ...
In the computation of flow fields about complex configurations, it is very difficult to construct a ...
Transonic flow fields about wing geometries are computed using an Euler/Navier-Stokes approach in wh...
The goal of this research was to further develop zonal methods and three dimensional procedures for ...
Recent advances in computing power and numerical solution procedures have enabled computational flui...
Computational Fluid Dynamics is beginning to play a major role in the design of aerospace vehicles. ...
An outline is presented for the creation of surface grids from primitive geometry data such as obtai...
A fast algorithm was developed for accurately generating boundary-conforming, three-dimensional, con...
In the past decade significant advances were made using flow field methods in the calculation of ext...
A fast computer program, GRID3C, was developed to generate multilevel three dimensional, C type, per...
The transonic Navier-Stokes code was used to simulate flow fields about isolated wings for workshop ...
The thin-layer Navier-Stokes equations are coupled with a zonal scheme (or domain-decomposition meth...
Important issues involved in working with complex geometries are discussed. Approaches taken to addr...
Grid generation and Euler flow about fighter aircraft are described. A fighter aircraft geometry is ...
The computation of flow over complex geometries, such as realistic aircraft configurations, poses di...
A suitable grid system for complex three dimensional configurations such as wing/body/nacelle shape ...
In the computation of flow fields about complex configurations, it is very difficult to construct a ...
Transonic flow fields about wing geometries are computed using an Euler/Navier-Stokes approach in wh...
The goal of this research was to further develop zonal methods and three dimensional procedures for ...
Recent advances in computing power and numerical solution procedures have enabled computational flui...
Computational Fluid Dynamics is beginning to play a major role in the design of aerospace vehicles. ...
An outline is presented for the creation of surface grids from primitive geometry data such as obtai...
A fast algorithm was developed for accurately generating boundary-conforming, three-dimensional, con...
In the past decade significant advances were made using flow field methods in the calculation of ext...
A fast computer program, GRID3C, was developed to generate multilevel three dimensional, C type, per...
The transonic Navier-Stokes code was used to simulate flow fields about isolated wings for workshop ...
The thin-layer Navier-Stokes equations are coupled with a zonal scheme (or domain-decomposition meth...
Important issues involved in working with complex geometries are discussed. Approaches taken to addr...
Grid generation and Euler flow about fighter aircraft are described. A fighter aircraft geometry is ...