Add to ORKGAn algebraic method is used to generate curvilinear body-fitted grids for an airfoil.The region exterior to the airfoil over which grids are to be generated is mapped to an approximate rectangle whose appropriate discretisation, gives the required grids in the physical plane. Two schemes to generate C-type grids using different transformations are given. A scheme to obtain O-type grid is also given. A listing of the cornputer program to generate C-grid where one of the coordinate curves is a family of parabolas is given in appendix.13
Algebraic procedures are described for the automatic generation of structured, single-block flow com...
An algorithm for the generation of hybrid prismatic/tetrahedral grids for complex 3-D geometries is ...
Generation of a viable coordinate system represents an important component of an isolated airfoil Na...
An algebraic method is used to generate curvilinear body-fitted grids for an airfoil.The region exte...
An algorithm is developed to obtain the grid sensitivity with respect to design parameters for aerod...
A new approach to construct high quality meshes for flow calculations is investigated in the context...
An algorithm is developed to obtain the grid sen� sitivity with respect to design parameters for aer...
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. ...
Direct numerical simulations of transitional and turbulent flows around airfoils at moderate and hig...
The-present work on grid generation is the Phase I of a project titled 'Hypersonic Flow Studies' tha...
The basic philosophy and techniques of the interactive parametric grid generation system Megacads ar...
This chapter focuses on three computer-aided geometric design (CAGD) techniques that are often neede...
The paper describes a technique for the generation of boundary-fitted curvilinear coordinate systems...
SIGLECopy held by FIZ Karlsruhe; available from UB/TIB Hannover / FIZ - Fachinformationszzentrum Kar...
Algebraic procedures are described for the automatic generation of structured, single-block flow com...
An algorithm for the generation of hybrid prismatic/tetrahedral grids for complex 3-D geometries is ...
Generation of a viable coordinate system represents an important component of an isolated airfoil Na...
An algebraic method is used to generate curvilinear body-fitted grids for an airfoil.The region exte...
An algorithm is developed to obtain the grid sensitivity with respect to design parameters for aerod...
A new approach to construct high quality meshes for flow calculations is investigated in the context...
An algorithm is developed to obtain the grid sen� sitivity with respect to design parameters for aer...
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. ...
Direct numerical simulations of transitional and turbulent flows around airfoils at moderate and hig...
The-present work on grid generation is the Phase I of a project titled 'Hypersonic Flow Studies' tha...
The basic philosophy and techniques of the interactive parametric grid generation system Megacads ar...
This chapter focuses on three computer-aided geometric design (CAGD) techniques that are often neede...
The paper describes a technique for the generation of boundary-fitted curvilinear coordinate systems...
SIGLECopy held by FIZ Karlsruhe; available from UB/TIB Hannover / FIZ - Fachinformationszzentrum Kar...
Algebraic procedures are described for the automatic generation of structured, single-block flow com...
An algorithm for the generation of hybrid prismatic/tetrahedral grids for complex 3-D geometries is ...
Generation of a viable coordinate system represents an important component of an isolated airfoil Na...