Add to ORKGA simple- approach has been developed to use the two13; dimensional grid generation method by solving elliptic partial differential equations to generate the three dimensional grid for wing-fuselage configurations. This simple method can be applied to generate grids for arbitrary fuselage fitted with any swept. wing with dihedral. Three dimensional transonic analysis code TWING, with approximate factorization (AF2) scheme has been suitably used as a flow solver. As an example, RAEx2014;WING-A with body-B2 configuration has been considered. The results obtained have been compared with available numerical and experimental results. It has been observed in the present computations that AF2 scheme is not sensitive to grid stretching
The main thrust of this paper has been the exploitation of Cartesian grids in the numerical solution...
An approximate factorization scheme based on the AF2 algorithm is presented for solving the three-di...
The object of the present work was to validate the two well known codes STWING and SFL022 to compute...
A simple- approach has been developed to use the two13; dimensional grid generation method by solvin...
A simple idea to generate grids for arbitrary shaped finite fuselage with a wing with twist and dihe...
Three dimensional transonic full potential equation has been solved in conservative and non-conserva...
The transonic full potential code using' body fitted coordinates with ADI/AF2 scheme is under develo...
The implicit approximate factorization scheme known as AF2 is investigated for application to the so...
The object of this report is to summarize the work done on 3D transonic flow computations during the...
A new approach to simulating transonic flow about transport configurations is briefly outlined. The ...
Full potential equation for two and three dimensional transonic flow has been considered. Emphasis h...
The goal of this research was to further develop zonal methods and three dimensional procedures for ...
Computational Fluid Dynamics is beginning to play a major role in the design of aerospace vehicles. ...
[[abstract]]A fast, conservative finite difference scheme for the full potential equation has been a...
report covers the Phase II progress in a two-phase effort to develop the full-potential finite-volum...
The main thrust of this paper has been the exploitation of Cartesian grids in the numerical solution...
An approximate factorization scheme based on the AF2 algorithm is presented for solving the three-di...
The object of the present work was to validate the two well known codes STWING and SFL022 to compute...
A simple- approach has been developed to use the two13; dimensional grid generation method by solvin...
A simple idea to generate grids for arbitrary shaped finite fuselage with a wing with twist and dihe...
Three dimensional transonic full potential equation has been solved in conservative and non-conserva...
The transonic full potential code using' body fitted coordinates with ADI/AF2 scheme is under develo...
The implicit approximate factorization scheme known as AF2 is investigated for application to the so...
The object of this report is to summarize the work done on 3D transonic flow computations during the...
A new approach to simulating transonic flow about transport configurations is briefly outlined. The ...
Full potential equation for two and three dimensional transonic flow has been considered. Emphasis h...
The goal of this research was to further develop zonal methods and three dimensional procedures for ...
Computational Fluid Dynamics is beginning to play a major role in the design of aerospace vehicles. ...
[[abstract]]A fast, conservative finite difference scheme for the full potential equation has been a...
report covers the Phase II progress in a two-phase effort to develop the full-potential finite-volum...
The main thrust of this paper has been the exploitation of Cartesian grids in the numerical solution...
An approximate factorization scheme based on the AF2 algorithm is presented for solving the three-di...
The object of the present work was to validate the two well known codes STWING and SFL022 to compute...