Preface vii
Introduction xi
Chapter 1. Truss Layout Optimization 1
1.1. Standard theory of mathematical programming 1
1.2. Governing equations of truss structures 3
1.3. Layout and topology optimization 7
1.3.1. Basic problem statement 7
1.3.2. Problem equivalence and numerical solution 11
1.4. Generalization 15
1.4.1. Self-weight and multiple loading 15
1.4.2. Compliance optimization 16
1.4.3. Volume optimization 17
1.4.4. Stress singularity 21
1.4.5. Local buckling singularity 25
1.5. Truss geometry and topology optimization 27
1.5.1. Optimization of nodal positions 27
1.5.2. Melting node effect 30
1.6. Concluding remarks 32
Chapter 2. Unified Formulation 33
2.1. Literature review 33
2.2. Disaggregation of equilibrium equations 36
2.3. Minimum volume problem 38
2.4. Minimum compliance problem 41
2.5. Reduced formulation for single loading 44
2.6. Nonlinear programming 46
2.6.1. Barrier problem 47
2.6.2. Sequential quadratic programming with trustregions 49
2.6.3. Verification test 51
2.7. Design settings 56
2.8. Concluding remarks 62
Chapter 3. Stability Considerations 65
3.1. Literature review 65
3.2. Lower bound plastic design formulation 69
3.3. Nominal force method for local stability 71
3.4. Local buckling criterion 75
3.5. Formulation including stability constraints 76
3.6. Numerical examples 78
3.6.1. Three-hinged arch 78
3.6.2. L-shaped frame 80
3.7. Concluding remarks 82
Chapter 4. Structural Design Applications 83
4.1. Reticulated dome 83
4.2. Lateral bracing of Winter's type column 86
4.3. Arch bridge 88
4.4. Suspension bridge 90
4.5. Dutch Maritime Museum 92
Conclusions and Future Prospects 99
Appendix 105
Bibliography 113
Index 135
Introduction
This introduction first describes lightweight structures in a historical context and points out current design issues. To tackle these challenges, section I.2 briefly discusses an empirical design process along with available methods for form finding and structural optimization. As a prelude to the novel method presented in this work, section I.3 introduces the conceptual framework of hanging models, plastic design and layout optimization leading to the computational design problem. The main achievements of the book are finally given in section I.4.
I.1. About lightweight structures
Structural design is an inseparable discipline of the art of building, whose governing factors are of a social, cultural, environmental, technical and financial nature. Given the considerable impact of the construction sector in terms of resources, today’s expectations are directed toward “meeting growing demand with limited resources”1. In this context, designing structures as light as possible may greatly contribute to more sustainability: by reducing the structural mass, we not only reduce the quantity of raw material, but we also decrease the embodied energy used for its production, transport, assembly, maintenance, and demolition or reuse, as well as the impact on the ground and foundations [KAN 07].
Lightweight structures are most suitable for covering wide spans with a limited amount of material. It is often argued that aesthetic values that make these structures visually appealing come from a functionally correct form, which mainly determines whether the system is able to withstand external loads without deteriorating serviceability, in addition to assessing the range of structural performance that can be attained. Mass and stiffness are the two fundamental criteria whose optimum is like systems of minimum energy in nature. To achieve the lowest mass-to-stiffness ratio, lightweight structures must be conceived as a force-differentiated system where tension, compression and shear are distributed on different components (cables, bars, membranes, etc.) [ERI 06]. If the structural form is inadequate, bending stiffness is required to compensate unbalanced forces, but this additional resistance adversely affects structural performance.
The emergence of lightweight structures can be traced back to the second half of the 19th Century. This period witnessed the advent of new material technologies such as steel, reinforced concrete, resistant glass and, later, fabric membrane. Together with advances in analysis and design tools, engineers and architects have been challenged to build increasingly lighter structures [LEW 03]. This has led to the development of the structural typologies depicted in Figure I.1. An early example was the Crystal Palace designed by Joseph Paxton for the Great Exhibition in London in 1851. The roof of 80 kg/m2 was a real progress at that time [KAW 11]. Another pioneering construction was the hyperboloid lattice tower by the Russian engineer Vladimir Shukhov in 1896. In the 1920s, Anton Tedesko first introduced reinforced concrete thin shells in the United States [HIN 04]. This expansion was pursued worldwide by Félix Candela [MOR 08], Heinz Isler [GAR 03] and André Paduart in Belgium [ESP 03]. The limit of lightness was achieved with tensile structures constructed of prestressed cable nets and fabric membranes; the strength coming from the anticlastic curvature of the geometric surface. A famous example of cable net is the roof of the Olympic stadium in Munich built in 1972, qualified as “architecture of the minimal” by its designer Frei Otto [OTT 96]. Pneumatic structures exhibit a close resemblance with tensile structures except that they are stabilized by the pressure of compressed air and prestressed cables. They also have an extremely low mass, as witnessed by the air-supported roof of 3 kg/m2 covering the US Pavillon at Expo’70.
Figure I.1. Classification of typologies of lightweight structures according to the actual stress state and the type of structural components
It should be mentioned that these historical examples were constructed in a period when labor was highly qualified and inexpensive, the requirements for safety and durability were more permissive, and when technical innovation gave meaning to the project. At the dawn of the 21st Century, a question arises: “the lighter, the better?” [KAW 11]. Although lightness remains the leading design criterion, this sole achievement is largely insufficient to cope with the increasing complexity of contemporary architecture. Nowadays, lightweight structures should be designed as a whole by including the multitude of design constraints. This will result in hybrid systems lying at the boundary of different typologies.
I.2. Design methodologies
The shaping process for lightweight structures is traditionally based on empirical knowledge and designers’ experience. An initial design is created, tested and updated in a series of structural analyses in order to achieve an optimal shape (Figure I.2(a)). However, each iteration requires engineers to manually generate the geometry of the analysis model. The task is time-consuming, error-prone and cumbersome for the designer. Furthermore, no matter how brilliant the designer is, it is often difficult to accurately predict and comprehend the effects of changing the geometry of lightweight structures without the risk of deteriorating the stiffness. This trial-and-error process can be advantageously pushed forward by computational design methods.
Still, two fundamental issues of lightweight structures must be thoroughly addressed to benefit from these developments: equilibrium and optimality [DES 11a]. The search for equilibrium is the basic requirement for safety, but it may transform a satisfactory design into a masterpiece when it is properly considered. The search for optimality is the never-ending task of improving the design while satisfying project constraints. Over the last 40 years, researchers have been continuously devising innovative methods to address these issues.
Figure I.2. Different kinds of design process with a) the conventional trial-and-error process, b) the structural form-finding process and c) the structural optimization process
Finding an equilibrium shape is the main purpose of structural form-finding methods. Given the boundary and external loading conditions, this state-to-design approach requires the designer to prescribe the internal forces to obtain the geometrical coordinates that solve the equilibrium equations (Figure I.2(b)). The literature covering structural form finding is briefly discussed in Appendix A1.1. Although structural efficiency may result as a welcome side effect (no optimality criterion is used, in fact), there are frequent situations in which we wish to impose geometrical constraints. In this case, form-finding methods are inadequate since the shape is the output of the process. Furthermore, stability issues that may considerably affect the optimal shape cannot be considered. Some strategies have been proposed [ZHA 06b, DES 10, DES 11c, RIC 13, QUA 13], but their scope is restricted to specific problems.
Finding an optimal shape is the ambitious task of structural optimization. The approach requires the designer to mathematically formulate the structural design problem as an optimization problem consisting of the minimization of an objective function subject to inequality and equality constraints. In the classical design-to-state (or nested) approach, the design variables are introduced in a dedicated structural analysis routine which computes the state variables. Based on these responses, an optimization algorithm iteratively updates the design toward the optimum (Figure I.2(c)). As a rule for selecting an optimization algorithm, the more intensive the local exploitation, the stronger the need for specialized information about the problem to be optimized. Deterministic methods are problem-specific and best suited for local search (these aspects will be discussed later in this book), whereas metaheuristics (see the discussion in Appendix A1.2) have broader search capabilities. Structural optimization problems are often very large (several thousand variables and constraints) and the design space comprises many local optima. Hence, deterministic methods might produce small improvements if the problem is not properly stated, whereas metaheuristics might be inefficient if no variable selection has been applied a priori. Furthermore, the variable nature of the structural layout causes singularities during the optimization process [RIC 12, DES 13b].
Although structural optimization methods have tremendous potential, we have to accept that the promise of these approaches is not easily realized. These persisting problems prevent their routine use by structural designers. Instead, the widespread use of computer-aided design tools has enabled the development of increasingly complex geometries in freeform architecture. In this long-awaited freedom of design, structural considerations were perceived as restraining the creativity of designers. As a consequence, structural engineers have been excluded from the preliminary shape design process and their role has been recentered on sizing and checking arbitrarily defined structures to meet the standard code requirement. Against all odds, a handful of structural designers still pursue the line of thought for unity and coherence between form and force in architecture. Former theories on structural design can inspire the development of creative, yet rigorous, strategies to empower this...