Design of geodesic dome structures.
Tofan, Mihai ; Tierean, Mircea ; Baltes, Liana 等
Abstract: This paper presents a MathCAD finite element application
for Fuller's dome structures. The dome's structure is
generated introducing
the radius of external sphere. For architectural reasons, some of the
theoretical nodes of structures can be omitted. The introduction of
material's properties and the geometrical parameters of the bars
are the next step. After the assemblage of the stiffness matrix, the
restraints and the forces are applied for several loading cases. The
nodal displacements are calculated and the distorted structure is drawn,
for each loading case. The structure's bars are checked at
traction, bending and buckling. The welded joins are also calculated and
the resonance frequencies of the dome.
Key words: FEA, simulation, structures, geodesic dome
1. INTRODUCTION
The geodesic dome structure was invented in 1947 by Richard
Buckminster Fuller (July 12, 1895-July 1, 1983). Even if domes have
existed for centuries, the geodesic domes are better than those because
they combine the sphere, the most efficient container of volume per
square meter, with the tetrahedron, which provides the greatest strength
for the least weight, or using different words "the most economical
momentary relationship among a plurality of points and events"
(http://www.thirteen.org/bucky/dare.html).
This geodesic dome uses a pattern of self-bracing triangles in a
pattern that gives maximum structural advantage, thus theoretically
using the least material possible (a "geodesic" line on a
sphere is the shortest distance between any two points).
The subject of this paper is the calculation program developed in
MathCAD for geodesic dome structures.
2. GEODESIC DOME GEOMETRY
According to the number of struts' distinct dimensions it is
possible to realize different geodesic geometries
(http://www.desertdomes.com). The simplest geometry has the same length
for all the struts and its name is "1v". The 1v dome is
actually an icosahedron (solid figure with twenty faces) with the 5
struts bottom removed. The structure with two different struts'
lengths (2v) is obtained removing 20 bars from the complete geodesic
sphere.
The subject of this paper is the structure with three different
struts' lengths (3v). The pattern for this structure contains nine
triangles (Figure 1). The analyzed structure has the outer sphere radius
of R=4.85 m.
[FIGURE 1 OMITTED]
The first step in geometry description of the structure is the
numbering of nodes. The top of the structure was labeled as 0 and each
level of triangles starts with the next number from the near right node
in counterclockwise. The 3D coordinates of the nodal points are obtained
applying the geodesic dome analytical relations into an Auto LISP
program. These coordinates are imported in MathCAD using READPRN
function and multiplied with the radius (Mathsoft, 2001).
Next, a nodal junction matrix was build, which defines the elements
of the structure. In this matrix the first line shows the start node and
the second line the arrival node. The structure defined in this way has
61 nodes and 150 elements. Now is time to introduce the struts'
geometry, which includes the dimensions of the cross section and
mechanical properties of the material: density, tensile and flexural Young modulus. Using these values the inertia characteristics are
calculated for each bar.
3. NODAL DISPLACEMENTS COMPUTING
Because the struts are fully constrained in nodes, the typical
element for this structure is the beam element. The relations are
explained using a simple rectangular element. The linear relation
between displacement and force can be explained using the relation:
[delta] = D x F, (1)
where: [delta]-displacements matrix;
D-compliance matrix;
F-forces matrix.
Considering the same cross sectional properties for all the
elements, the local stiffness matrix (the inverse of compliance matrix)
for each beam can be very easily built using the formula (Tofan et al.,
1995):
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (2)
where: [[alpha].sub.j] = A x [L.sup.2.sub.j]/Iz, [beta] = Iy/Iz,
[tau] = G x It/2E x Iz;
A-cross sectional area;
Iz, Iy, It-inertia characteristics of bar;
E, G--tensile and flexural Young modulus;
[L.sub.j]-bar's length.
To transport this local stiffness in the global coordinate system
(the center of the sphere) it is necessary to multiply them with the
rotation and translation operators, proper for each bar. The assembling
of the local stiffness into the global stiffness matrix can be realized
using the positional incidence.
[FIGURE 2 OMITTED]
After this step, the fixing structure will be added and the outer
forces are introduced in nodes. All the nodes from the lowest level are
considered fixed into foundation. For the rest of the nodes, six loading
values correspond: the first three refer to forces and the rest of them
to moments. After that, the nodal displacements are calculated (six for
each node) by multiplying the inverse of stiffness matrix with the outer
forces matrix. These nodal displacements draw the distorted structure
(Figure 2), amplified by [10.sup.3].
4. STRESSES AND VIBRATION CHECKING
Having the displacements of each node, the nodal forces are
obtained, in the global coordinate system and also the forces for each
element. Using these forces (six for each bar edge) the stresses that
affect the struts are determined. For each bar the Von Mises stresses
and buckling are verified.
The eigenfrequencies of the structure (Figure 3) that shows the
ability of the structure to avoid collapses caused by earthquakes and
winds are also calculated.
For the analyzed structure three types of loadings are considered:
* wind, 730 N/[mm.sup.2];
* snow, 2440 N/[mm.sup.2];
* gravitational loading of the bars and ceiling; applied for three
kinds of structures realized from:
* rectangular pinewood bars (150x50 mm) with end steel connectors;
* aluminum tube ([phi]0x5 mm);
* stainless steel tube ([phi]60x5 mm), the last two welded on
spheres connectors.
The elements are verified considering three loading hypothesis:
* gravitational loading plus wind force for all the free nodes;
* gravitational loading for all free nodes plus snow loading on
upper two triangle levels;
* gravitational loading plus wind force for all free nodes plus
snow loading on upper two triangle levels.
The values obtained for the worst loading case are presented in
table 1.
[FIGURE 3 OMITTED]
If the struts are made of pinewood, special connectors at
bars' ends are necessary. These connectors are made of steel tube
([phi]133x8 mm) welded with two steel strips for each beam. Using two
bolts the struts are joined to node. Figure 4 presents the Von Mises
stresses map obtained using Design Star F.E.A. software. Based on
symmetry only half of the connector was modeled. For meshing, the 5 mm
tetragonal solid element was used. The maximum stress is
9.364x[10.sup.7] Pa.
[FIGURE 4 OMITTED]
5. CONCLUSION
The presented programs show the deformed structures, the
displacements' values, the bars stresses and the eigenfrequencies
of the geodesic dome structure. Simply introducing the radius of the
sphere, the material characteristics and bars' geometry, the
problem is solved.
This program shows that local loads are distributed throughout the
geodesic dome, using the entire structure. Geodesic domes get stronger,
lighter and cheaper per unit of volume as their size increases, just the
opposite of conventional building.
For the chosen example the top displacement is approximately 1 mm,
the stresses are lower than admissible values and the eigenfrequencies
are greater than the value proper to earthquakes and winds.
Due to the simplicity and this high velocity, the program is easy
to implement in any type of calculation for geodesic dome structures,
avoiding the laboriously methodology of the modeling, introducing data
and calculation, claimed by commercial programs for F.E.A.
6. REFERENCES
Tofan, M.C., Goia, I., Tierean, M.H. & Ulea, M. (1995).
Deformatele structurilor (Structure's strains), Editura Lux Libris,
ISBN 973-96854-2-0, Brasov, Romania
Mathsoft, Inc. (2001) MathCAD User's Guide, Cambridge, MA
Available from: http://www.desertdomes.com Accessed: 2007-07-17
Available from: http://www.thirteen.org/bucky/dare.html Accessed:
2007-07-17
Table 1. Values obtained for the worst loading case.
Maximum Top
Von Mises stress displacement
Material Pa mm
Rectangular pine bars 3.26 x [10.sup.5] 0.965
Aluminum tube 1.24 x [10.sup.6] 1.096
Stainless steel tube 1.45 x [10.sup.6] 0.557
Minimum Buckling
eigenfrequency safety factor
Material Hz
Rectangular pine bars 15.438 9.078
Aluminum tube 18.675 26.95
Stainless steel tube 19.478 29.17