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The cuts are used to join the disconnected components of the domain boundary in order to reduce their number. Theoretically, this operation can allow one to generate a single coordinate transformation in a multiply connected domain. The choice of the grid topology in a block depends on the structure of the solution, the geometry of the domain, and, in the case of continuous or smooth grid-line communication, on the topology of the grid in the adjacent block as well.

For complicated domains, such as those near aircraft surfaces or turbines with a large number of blades, it is dicult to choose the grid topology of the blocks, because each component of the system wing, fuselage, etc. In any specic case, these conditions are determined by features of the computer, the methods of grid generation available, the topology and conditions of interaction of the blocks, the numerical algorithms, and the type of data to be obtained.

One of the main requirements imposed on the grid is its adaptation to the solution. Multidimensional computations are likely to be very costly without the application of adaptive grid techniques. The basic aim of adaptation is to enhance the eciency of numerical algorithms for solving physical problems by a special nonuniform distribution of grid nodes.

The appropriate adaptive displacement of the nodes, depending on the physical solution, can increase the accuracy and rate of convergence and reduce oscillations and the interpolation error. In addition to adaptation, the construction of locally structured grids often requires the coordinate lines to cross the boundary of the domain or the surface in an orthogonal or nearly orthogonal fashion. The orthogonality at the boundary can greatly simplify the specication of boundary conditions. Also, a more accurate representation of algebraic models of turbulence, the equations of a boundary layer, and parabolic NavierStokes equations is possible in.

If for grids of O and C-type the coordinate lines are orthogonal to the boundary of each block and its interior cuts, the global block-structured grid will be smooth.

Principles of grid generation - Wikipedia

It is also desirable for the coordinate lines to be orthogonal or nearly orthogonal inside the blocks. This will improve the convergence of the dierence algorithms, and the equations, if written in orthogonal variables, will have a simpler form. For unsteady gas-dynamics problems, some coordinates in the entire domain or on the boundary are required to have Lagrange or nearly Lagrange properties. With Lagrangian coordinates the computational region remains xed in time and simpler expressions for the equations can be obtained in this case.

It is also important that the grid cells do not collapse, the changes in the steps are not too abrupt, the lengths of the cell sides are not very dierent, and the cells are ner in any domain of high gradient, large error, or slow convergence.


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Requirements of this kind are taken into account by introducing quantitative and qualitative characteristics of the grid, both with the help of coordinate transformations and by using the sizes of cell edges, faces, angles, and volumes. The characteristics used include the deviation from orthogonality, the Lagrange properties, the values of the transformation Jacobian or cell volume, and the smoothness and adaptivity of the transformation.

For cell faces, the deviation from a parallelogram, rectangle, or square, as well as the ratio of the area of the face to its perimeter, is also used. Overset grids are exempt from this restriction. With the overset concept the blocks are allowed to overlap, which signicantly simplies the problem of the selection of the blocks covering the physical region.

In fact, each block may be a subdomain which is associated only with a single geometry or physical feature.

The global grid is obtained as an assembly of structured grids which are generated separately in each block. These structured grids are overset on each other, with data communicated by interpolation in overlapping areas of the blocks Fig. These meshes are widely used for the numerical analysis of boundary value problems in regions with a complex geometry and with a solution of complicated structure.

They are formed by joining structured and unstructured grids on dierent parts of the region or surface. Commonly, a structured grid is generated about each chosen boundary segment.

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These structured grids are required not to overlap. The remainder of the domain is lled with the cells of an unstructured grid Fig. This construction is widely applied for the numerical solution of problems with boundary layers. The chief practical diculty facing grid generation techniques is that of formulating satisfactory techniques which can realize the users requirements. Grid generation techniques should develop methods that can help in handling problems with multiple variables, each varying over many orders of magnitude. These methods should be capable of generating grids which are locally compressed by large factors when compared with uniform grids.

The methods should incorporate specic control tools, with simple and clear relationships between these control tools and characteristics of the grid such as mesh spacing, skewness, smoothness, and aspect ratio, in order to provide a reliable way to inuence the eciency of the computation. And nally, the methods should be computationally ecient and easy to code. A number of techniques for grid generation have been developed. Every method has its strengths and its weaknesses. Therefore, there is also the question of how to choose the most ecient method for the solution of any specic.

The goal of the development of these methods is to provide eective and acceptable grid generation systems. The generation of these grids can be performed by a number of approaches and techniques. Many of these methods are specically oriented to the generation of grids for the nite-dierence method.

A boundary-tted coordinate grid in the region X n is commonly generated rst on the boundary of X n and then successively extended from the boundary to the interior of X n. This process is analogous to the interpolation of a function from a boundary or to the solution of a dierential boundary value problem. On this basis there have been developed three basic groups of methods of grid generation: 1 algebraic methods, which use various forms of interpolation or special functions; 2 dierential methods, based mainly on the solution of elliptic, parabolic, and hyperbolic equations in a selected transformed region; 3 variational methods, based on optimization of grid quality properties.

Algebraic methods are simple; they enable the grid to be generated rapidly and the spacing and slope of the coordinate lines to be controlled by the blending coecients in the transnite interpolation formulas. However, in regions of complicated shape the coordinate surfaces obtained by algebraic methods can become degenerate or the cells can overlap or cross the boundary. Moreover, they basically preserve the features of the boundary surfaces, in particular, discontinuties.

Algebraic approaches are commonly used to generate grids in regions with smooth boundaries that are not highly deformed, or as an initial approximation in order to start the iterative process of an elliptic grid solver.

Basics of Grid Generation for CFD Analysis

The interior coordinate lines derived through these methods are always smooth, being a solution of these equations, and thus discontinuties on the boundary surface do not extend into the region. The use of parabolic and elliptic systems enables. Elliptic equations are also used to smooth algebraic or unstructured grids. In practice, hyperbolic equations are simpler then nonlinear elliptic ones and enable marching methods to be used and an orthogonal system of coordinates to be constructed, while grid adaptation can be performed using the coecients of the equations.

Meshing for Control, Quality, and Automation

However, methods based on the solution of hyperbolic equations are not always mathematically correct and they are not applicable to regions in which the complete boundary surface is strictly dened. Therefore hyperbolic methods are mainly used for simple regions which have several lateral faces for which no special nodal distribution is required. Hyperbolic generation is particularly well suited for use with the overset grid approach. The marching procedure for the solution of hyperbolic equations allows one to decompose only the boundary geometry in such a way that neighboring boundary grids overlap.

Volume grids will overlap naturally if sucient overlap is provided on the boundary. In practice, a separate coordinate grid around each subdomain can be generated by this approach. Variational methods take into account the conditions imposed on the grid by constructing special functionals dened on a set of smooth or discrete transformations.


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  • A compromise grid, with properties close to those required, is obtained with the optimum transformation for a combination of these functionals. At present, variational techniques are not widely applied to practical grid generation, mainly because their formulation does not always lead to a wellposed mathematical problem.

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    However, the variational approach has been cited repeatedly as the most promising method for the development of future grid generation techniques, owing to its underlying, latent, powerful potential. There are, fundamentally, three approaches to the generation of unstructured grids: octree methods, Delaunay procedures, and advancing-front techniques. Then the cubes containing segments of. The cells intersecting the body surfaces are formed into irregular polygonal cells. The grid generated by this octree approach is not considered as the nal one, but serves to simplify the geometry of the nal grid, which is commonly composed of tetrahedral or triangular cells built from the polygonal cells and the remaining cubes.

    The main drawback of the octree approach is the inability to match a prescribed boundary surface grid, so the grid on the surface is not constructed beforehand as desired but is derived from the irregular volume cells that intersect the surface.

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    Another drawback of the grid is its rapid variation in cell size near the boundary. In addition, since each surface cell is generated by the intersection of a hexahedron with the boundary there arise problems in controlling the variation of the surface cell size and shape. The points can be generated in two ways; they can be dened at the start by some technique or they can be inserted within the tetrahedra as they are created, starting with very coarse elements connecting boundary points and continuing until the element size criteria are satised.