Bezier and B-spline patches are popular tools in surface modeling. With these methods, a surface is represented by the tensor product of univariate approximations. The extension of this concept to three dimensions is obvious and can be applied to the problem of grid generation. This report will demonstrate how three dimensional patches can be used in solid modeling and in the generation of grids. Examples will be given demonstrating the ability to generate three dimensional grids directly from a wire frame without having to first set up the boundary surfaces. Many geometric grid properties can be imposed by the proper choice of the control net

Mastin, C. Wayne

English

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APPLICATION OF THREF_,-DIMENSIONAL Bl_ZIER PATCHES
IN GRID GENERATION *
C. Wayne Mastin
Mississippi State University
Mississippi State, MS
SUMMARY
B_zier and B-spline patches are popular tools in surface modeling. With these methods,
a surface is represented by the tensor product of univariate approximations. The extension
of this concept to three-dimensions is obvious and can be applied to the problem of grid
generation. This report will demonstrate how three-dimensional patches can be used in solid
modeling and in the generation of grids. Examples will be given demonstrating the ability
to generated three-dimensional grids directly from a wire frame without having to first set
up the boundary surfaces. Many geometric grid properties can be imposed by the proper
choice of the control net.
INTRODUCTION
Free-form modeling of surfaces has been the main objective in the field of computer aided
geometric design. Rational B_zier curves and surfaces have been used extensively for surface
modeling. With this method, as well as most other methods of curve and surface modeling,
the geometric object is defined using a set of points and a set of basis functions. In the case
of surfaces a tensor product basis is used to construct the basis functions for generating a
surface patch. Precisely how the basis functions are used in the surface generation depends
on the desired properties of the surface. In particular, it depends on whether the set of
points that is used to describe the object is to be interpolated as a wire frame for building
the surface or is to be a control net to describe the general shape of the surface. It is the
first method, usually associated with Coons patches, that will be used to develop a solid
modeling technique. However, either concept can be generalize to three dimensions. In
"Work supported by NASA Grant NSG 1577.
(NASA-CR-189000) APPLICATION OF
TUR_E-OIM_NSIONAL BELIER PATCHES IN GRID
GENERATION (_ississippi Stake Univ.) 9 p
CSCL 12A
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N92-24350
Unclas
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https://ntrs.nasa.gov/search.jsp?R=19920015107 2020-03-17T12:08:07+00:00Z
fact, the patches, which probably should be referred to as blocks in the three-dimensional
analogue, are actually defined by constructing a control net.
The purpose of this report is to investigate the concept of free-form modeling of surfaces
and apply the idea to the field of grid generation. In the following sections, the generalization
of rational B_zier curves to three dimensions is developed and used in the construction of
three-dimensional grids. The development is analogous to that used to generate surfaces and
follows the terminology and notation of Farin [1]. No doubt the extension of one-dimensional
basis functions to arbitrary tensor products in any dimension was known to exist from the
earliest development of tensor product surfaces, however, the first application of the concept
in solid modeling appeared to be in the paper of Saia et aI. [2]. Another use of three-
dimensional basis functions was also note by Farin.
Several examples of three-dimensional grids constructed from wire frame descriptions are
presented. Although no detailed analysis of the quality of the generated grid has been done,
it has been shown that in most cases the grid is very close to the grid which is constructed
using transfinite interpolation.
RATIONAL Bl_ZIER PATCHES
A three-dimensional solid is given by a wire frame description. The blocks of the wire
frame are filled in with patches and a grid is constructed in each patch. Three-dimensional
grids are constructed using the tensor products of one-dimensional basis functions. The basis
functions for the rational B_zier curve of degree n are given as
R?(t) =
E?=ow B (t)
where the B_' are the Bernstein polynomials defined as
B'_(t)= (n) ti(1-t)'_-i'i
The weight parameters wi can be used to cause grid clustering near points of the wire frame.
A three-dimensional patch can be constructed from a control net. If the basis functions
are of degree l, m and n, then the points of the control net can be denoted as a three-
dimensional array {bi,/,k},i = 0,..-,I, j = 0,.-.,m, k = 0,...,n. The points of the patch
are defined using the tensor product basis functions and the points of the control net. The
points of the patch are describedby the parametric equation
l Err
b(r,s,t) = _ _ _-_ bij,kR_(r)R?(s)R_(t)
i=O j=O k=O
As in the two dimensions, the case of most interest is when l = m =- n = 3. For it is
then that we have enough control points to ensure continuity of grid line slopes between
patches or specify any other type of boundary condition for the grid line slopes. Therefore,
in the grid construction in the next section, only rational tricubic B_zier basis functions are
implemented.
GRID CONSTRUCTION
The grid construction begins with the input of the coordinates of a wire flame which
describes the general shape of the three-dimensional region to be gridded. Along with the
point coordinates, there is also input information describing the type of grid line continuity
or discontinuity that is to be imposed at the wire frame points. This information is used to
prdscribe the location of the control points in each block of the wire frame. The description of
a rational cubic B_zier curve requires four points, including the two end points of the curve.
Therefore each block of the wire frame will require a total of 64 control points including
the four vertices on the wire frame. These control points are chosen so that the grid lines
have the desired continuity or direction property requested by the input information. So as
not to generate an excessive amount of input, the directions of the grid lines were computed
using differences of coordinates computed on the wire frame. By using various combinations
of central and one-sided difference quotients, the grid lines can be constructed so that they
have a discontinuous slope or pass smoothly through the points of the wire frame. Except
for the boundary points, a control point is needed on each side of the input point in each
of the coordinate directions. These control points indicate the direction of the grid line as
it enters and leaves the point. The following list indicates the different types of conditions
that have been implemented.
1. Weighted central differences used in both directions.
2. Forward difference used on both sides.
3. Backward difference used on both sides.
4. Backward used going toward point, forward used leaving point.
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5. Forward or backward differences at a boundary point.
6. Periodic conditions.
7. Rounded corners.
8. Orthogonal grid lines at a symmetry plane.
The weighting referred to in condition 1 was found to give a better value for the slope.
The usual central difference can be formulated as the average of a forward and a backward
difference. Here a weighted average of a forward and a backward difference is used where
the weighting depends on the distance to the two neighboring points on the wire frame.
Several examples are presented to demonstrate the use of the three-dimensional B_zier
patches in grid generation. The first example is plotted in Figure 1. The wire frame model
describes a simple duct with a varying cross section. The rounded corner option is used
to change the duct from a rectangular shape to an oval shape. The plots of the interior
grid surfaces show a uniform distribution of grid points. The weights in the basis functions
were all set to one for this example. The second example is more interesting. A minimal
number of points is used to describe a wing and part of a fuselage. The bulge below the
wing is representative of a faired over engine inlet. Weighting of the basis functions has been
used to cluster grid points near the wing/fuselage configuration. The symmetry plane was
constructed through the center of the fuselage. Grid lines axe orthogonal to the symmetry
plane. Different control point directions at the wing tips resulted in the corners on the
aircraft surface. The wire frame and several gridded surfaces are shown in Figure 2. The
last example is another aircraft configuration. The same number of points as in the previous
exampIe is used to model a high speed aircraft. Only the basic wing fuselage geometry is
modeled. The grid, plotted in Figure 3, demonstrates the capability of dealing with a polar
type of axis and a periodic coridition. The sparsity in the number of points which describes
the geometry is evident in the wire frame.
There are many three-dimensional grid generation methods that can generate a volume
grid from a given surface grid. Thus the question might be asked as to how the grids
constructed above using the three-dimensional solid modeling technique differs from the
interior grid which would be constructed from a set of bounding surface grids. In an attempt
to answer this question, the boundary grids from Figure 3 were used to generate interior grids
by transfinite interpolation. The grids constructed by the two methods are not identical,
but as can be seen in Figure 4, they are nearly the same, and it would be difficult to say
which method generates a better grid. Either grid could be improved by applying an elliptic
method to reduce skewness. The grid distribution could also be controlled by adding interior
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interpolation surfaces in the case of the transfinite interpolation, or by adding points to the
wire frame representation in the case of the BSzier grid.
In all of these examples, a uniform knot spacing was used in each patch, however, nonuni-
form rational B_zier functions could be used or one could use rational B-splines. In any case
the basic concept is a straightforward generalization of the surface construction procedure.
One point that is of both practical and mathematical interest has not been treated in this
report. That is the three-dimensional analogue of the well-known twist problem in surface
modeling. The continuity in the coordinate gradients is not sufficient to uniquely determine
all of the control points, and the manner in which these points are chosen determines whether
the surface has the correct shape near the vertices of the patch. In our computations, it has
been assumed that the mixed derivatives vanish, which in surface modefing is known to result
in flat regions near the corners. One of several twist models could have been used, but there
would stilI be Ieft the four interior control points of the bIock to be determined. Therefore,
until there is a reasonable three-dimensional twist model available, it was decided to simply
neglect the mixed derivative effects ..........
CONCLUSIONS
The results of this report show that solid modeling techniques using three-dimensional
rational B_zier functions can be used to generate grids in a simple one-step procedure. Many
different types of configurations and edge and face treatments can be included in the model.
The complexity of the geometric model is only limited by the amount of input that is desired.
This solid modeling technique is designed for free-form solids where a general shape or design
is to be modeled rather than for constructing a solid with precisely defined edges or faces.
REFERENCES
1 Gerald Farin, Curves and Surfaces for Computer Aided Geometric Design: A Practical
Guide, Second Edition, Academic Press, San Diego, 1990.
2 A. Saia, M. S. Bloor, and A. De Pennington, "Sculptured Solids in a CSG Based
Geometric Modelling System", in The Mathematics of Surfaces H, R. R. Martin, Ed.,
Clarendon, Oxford, 1987.
1 J m
Figure 1. Wire frame and surface grids for a duct with a varying cross section.
Figure 2. Wire frame and surfacegrids for a wing and part of a fuselage.
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Figure 3. Wire frame and surface grids for a high speed aircraft.
Figure 4. A comparisonof 3D B_zier grids (solid lines) and transfinite interpolation grids
(dashlines).
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Application of three-dimensional Bezier patches in grid generation

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