The main thrust of this paper has been the exploitation of Cartesian grids in the numerical solution of transonic full potential equation. Notwithstanding the present-day popularity for the use of body-wrapped coordinate systems in the context of Computational Fluid Dynamics, concerted effort has been made here to work with Cartesian grids for a variety of flow situations: aerofoils, axisymmetric flows, wings and wing-body combinations. One reason for this is that the codes based on these grids become amenable to computers with limited storage and speed. Several cases are presented here for each of the above flow situations. The results clearly demonstrate the efficacy of Cartesian grids for dealing with complex geometries and also undersco...
Computational Fluid Dynamics is beginning to play a major role in the design of aerospace vehicles. ...
A numerical scheme utilizing a chimera zonal grid approach for solving the full potential equation i...
The urgent need for dramatic reductions in aircraft design cycle time is focusing scrutiny upon all ...
The main thrust of this paper has been the13; exploitation of Cartesian grids in the numerical13; so...
The full-potential equation in non-conservative form is solved in stretched Cartesian grid to obtain...
A code has been developed to compute axisymmetric Viscous13; transonic flow. An important feature of...
Results are presented here tor viscous transonic flow over13; aerofoils to demonstrate the capabilit...
This Note covers attempts to extend an existing two dimensional transonic code, TRADE 1, in Cartesia...
Various forms of FP (full potential) equation, spatial differencing schemes, and iterative schemes a...
A modification is introduced in the Cartesian grid construction for analysis of flow past swept wing...
A numerical technique for analyzing transonic airfoils is presented. The method employs the basic fe...
The Cartesian grid method is an alternative to the existing methods to solve a physical problem gove...
A simple- approach has been developed to use the two13; dimensional grid generation method by solvin...
A novel approach of automated hybrid Cartesian-body ¯tted grid (HCBFG) for simulations of °uid °ows ...
A novel grid-stitching algorithm has been developed for generating Cartesian-like grids for viscous ...
Computational Fluid Dynamics is beginning to play a major role in the design of aerospace vehicles. ...
A numerical scheme utilizing a chimera zonal grid approach for solving the full potential equation i...
The urgent need for dramatic reductions in aircraft design cycle time is focusing scrutiny upon all ...
The main thrust of this paper has been the13; exploitation of Cartesian grids in the numerical13; so...
The full-potential equation in non-conservative form is solved in stretched Cartesian grid to obtain...
A code has been developed to compute axisymmetric Viscous13; transonic flow. An important feature of...
Results are presented here tor viscous transonic flow over13; aerofoils to demonstrate the capabilit...
This Note covers attempts to extend an existing two dimensional transonic code, TRADE 1, in Cartesia...
Various forms of FP (full potential) equation, spatial differencing schemes, and iterative schemes a...
A modification is introduced in the Cartesian grid construction for analysis of flow past swept wing...
A numerical technique for analyzing transonic airfoils is presented. The method employs the basic fe...
The Cartesian grid method is an alternative to the existing methods to solve a physical problem gove...
A simple- approach has been developed to use the two13; dimensional grid generation method by solvin...
A novel approach of automated hybrid Cartesian-body ¯tted grid (HCBFG) for simulations of °uid °ows ...
A novel grid-stitching algorithm has been developed for generating Cartesian-like grids for viscous ...
Computational Fluid Dynamics is beginning to play a major role in the design of aerospace vehicles. ...
A numerical scheme utilizing a chimera zonal grid approach for solving the full potential equation i...
The urgent need for dramatic reductions in aircraft design cycle time is focusing scrutiny upon all ...