We use cookies to distinguish you from other users and to provide you with a better experience on our websites. Close this message to accept cookies or find out how to manage your cookie settings.
To save content items to your account,
please confirm that you agree to abide by our usage policies.
If this is the first time you use this feature, you will be asked to authorise Cambridge Core to connect with your account.
Find out more about saving content to .
To save content items to your Kindle, first ensure [email protected]
is added to your Approved Personal Document E-mail List under your Personal Document Settings
on the Manage Your Content and Devices page of your Amazon account. Then enter the ‘name’ part
of your Kindle email address below.
Find out more about saving to your Kindle.
Note you can select to save to either the @free.kindle.com or @kindle.com variations.
‘@free.kindle.com’ emails are free but can only be saved to your device when it is connected to wi-fi.
‘@kindle.com’ emails can be delivered even when you are not connected to wi-fi, but note that service fees apply.
This chapter introduced algebraic formulations as an innovative approach to 2DGS and 3DGS. These formulations capture the essence of the reciprocal relationship, representing the dual diagram algebraically. While requiring deeper insight into reciprocity, this method surpasses traditional approaches in its potency. With the aid of modern computational tools, we can efficiently navigate the solution space of these equations. The resultant algebraic framework promises increased efficiency, flexibility, and precision, enhancing our understanding of the relationship between form and force. Such advancements prove invaluable not only for academic pursuits but also for practical applications.
The method of Algebraic graphic statics comes with certain limitations. Primarily, it’s suited for linear static issues and linear constraints. Handling more intricate problems, such as the previously mentioned constraints on face areas, might not be straightforward. Such challenges may require quadratic functions, increasing the computational effort and cost for solutions. In terms of the implementation, although the data structure allows self-intersecting faces and cells to exist through later manipulation, the initial construction of the data structure cannot accept self-intersecting surfaces, i.e., all cells in the starting primal diagram need to be convex; otherwise, the topology cannot be detected and defined properly.
We invite the interested reader to visit other related topics under graphic statics, including vector-based 3D graphic statics \cite{Cremona1890,EPFL-CONF-218827,D'Acunto_2019}, and approaches using projections of polyhedral systems to higher dimensions and back by \cite{Konstantatou} and \cite{Baranyai2021}. Furthermore, \cite{Lee2018} proposed a method called \textit{Disjointed Force Polyhedra} where the equilibrium of the system was computed by constructing a single convex polyhedron for each node using Extended Gaussian Image algorithm, and then areas of the adjacent faces have matching areas but are allowed to have different shapes \cite{Lee2018,Lee2018phd}. In \cite{mcrobie_2016_minkowski}, a methodology was introduced for the computation and visualization of the Maxwell (in two dimensions) and Rankine (in three dimensions) diagrams that are reciprocal to a truss subjected to load. The formulation of these reciprocals is grounded in the Minkowski summation of the polyhedral stress functions inherent to both the original and the reciprocal diagrams. This approach aligns seamlessly with 3D graphic statics that utilize polyhedral reciprocal diagrams.
This chapter introduces compression-only form finding in both 2D and 3D. The properties of primitive constrained funicular forms in 2D and 3D are explained. The step-by-step procedures for constrained form finding for a single applied load in 2D and 3D are provided. The form-finding process is then extended from a single applied load to a non-concurrent system of loads, for instance, a series of parallel applied loads. We show how the form and force diagrams can be combined using the Minkowski sum to check the correctness of funicular construction. The relationship between the applied loads and the number of non-concurrent loads in polyhedral systems is explained. A design technique by subdividing the applied loads is introduced that yields a variety of load networks and, thus, shells with various topologies. Besides, the effect of support locations in 3D is illustrated using multiple examples. We provide examples to show an approach to controlling the width of funicular forms in 3D and constraining a funicular form’s height. The topic of the three-hinged arch in 2D and 3D is introduced, and the construction of overlaying funicular geometries for asymmetric loading scenarios is then explained.
In this paper, we develop an analytical model to investigate the generation of instability waves triggered by the upstream acoustic forcing near the nozzle lip of a supersonic jet. This represents an important stage, i.e. the jet receptivity, of the screech feedback loop. The upstream acoustic forcing, resulting from the shock-instability interaction (SII), reaches the nozzle lip and excites new shear-layer instability waves. To obtain the newly excited instability wave, we first determine the scattered sound field due to the upstream forcing using the Wiener–Hopf technique, with the kernel function factored using asymptotic expansions and overlapping approximations. Subsequently, the unsteady Kutta condition is imposed at the nozzle lip, enabling the derivation of the dispersion relation for the newly excited instability wave. A linear transfer function between the upstream forcing and the newly excited instability wave is obtained. We calculate the amplitude and phase delay in this receptivity process and examine their variations against the frequency. The analytically obtained phase delay enables us to evaluate the phase condition for jet screech and predict the screech frequency accordingly. The results show improved agreement with the experimental data compared with classical models. It is hoped that this model may help in developing a full screech model.
When an oblate droplet translates through a viscous fluid under linear shear, it experiences a lateral lift force whose direction and magnitude are influenced by the Reynolds number, the droplet’s viscosity and its aspect ratio. Using a recently developed sharp interface method, we perform three-dimensional direct numerical simulations to explore the evolution of lift forces on oblate droplets across a broad range of these parameters. Our findings reveal that in the low-but-finite Reynolds number regime, the Saffman mechanism consistently governs the lift force. The lift increases with the droplet’s viscosity, aligning with the analytical solution derived by Legendre & Magnaudet (Phys. Fluids, vol. 9, 1997, p. 3572), and also rises with the droplet’s aspect ratio. We propose a semi-analytical correlation to predict this lift force. In the moderate- to high-Reynolds-number regime, distinct behaviours emerge: the $L\hbox{-}$ and $S\hbox{-}$mechanisms, arising from the vorticity contained in the upstream shear flow and the vorticity produced at the droplet surface, dominate for weakly and highly viscous droplets, respectively. Both mechanisms generate counter-rotating streamwise vortices of opposite signs, leading to observed lift reversals with increasing droplet viscosity. Detailed force decomposition based on vorticity moments indicates that in the $L\hbox{-}$mechanism-dominated regime for weakly to moderately viscous droplets, the streamwise vorticity-induced lift approximates the total lift. Conversely, in the $S\hbox{-}$mechanism-dominated regime, for moderately to highly viscous droplets, the streamwise vorticity-induced lift constitutes only a portion of the total lift, with the asymmetric advection of azimuthal vorticity at the droplet interface contributing additional positive lift to counterbalance the $S\hbox{-}$mechanism’s effects. These insights bridge the understanding between inviscid bubbles and rigid particles, enhancing our comprehension of the lift force experienced by droplets in different flow regimes.
The chapter expanded on the definition, meaning, and application of Geometric Degrees of Freedom (GDoF) of the form and force diagrams in Polyhedral Graphic Statics. The number of independent edges in the network is the GDoF of a network of closed polygons/polyhedrons. An independent edge is an edge whose length can be independently chosen in constructing a network. These edges then determine the lengths of the rest of the edges in the network.
The geometric degree of freedom has different applications in the form and force diagrams. The GDoF of the force diagram in 2D and 3D allows exploring the static degrees of indeterminacies in the funicular form; the GDoF of the global force polygon/polyhedron corresponds to the external degrees of static indeterminacies in the funicular form.
Controlling the GDoF of a force diagram allows for removing reaction forces or applied loads in the boundary condition of a funicular form. This control can redistribute the internal forces in the structure’s members, e.g., from compression to tension, without changing the geometry of the funicular form and lead to exciting design options.
Like the force diagram, the form diagram also has geometric degrees of freedom. Using geometric degrees of freedom to manipulate the form diagram does change the form’s configuration but does not change the force magnitude and the equilibrium of forces in the system. Meanwhile, it opens the door to various funicular solutions ranging from compression-only to compression-and-tension combined systems.
Identifying the exact number of GDoF for both form and force diagrams in 3D is not a trivial task. It requires an algebraic formulation of the problem.
This paper provides an overview of the current status of ultrafast and ultra-intense lasers with peak powers exceeding 100 TW and examines the research activities in high-energy-density physics within China. Currently, 10 high-intensity lasers with powers over 100 TW are operational, and about 10 additional lasers are being constructed at various institutes and universities. These facilities operate either independently or are combined with one another, thereby offering substantial support for both Chinese and international research and development efforts in high-energy-density physics.
In this chapter, we showed the broader application of Polyhedral Graphic statistics in other fields of science and briefly introduced research directions and topics that go beyond the polyhedral limitations of this method. Particularly, we show a research project in which graphical methods were used to analyze the structural pattern of a dragonfly wing. The result was then combined with machine learning methods to generate the structure of a wing of an airplane with enhanced out-of-plane performance. We also visited applications in the design of strut-and-tie structures for referenced concrete and its further application in designing multi-material structural components where the direction of the deposition of material is adjusted with respect to the internal force flow to maximize mechanical performance. The application of Polyhedral Graphic Statics was shown in the design of cellular solids and briefly discussed how particular subdividing of the force diagram can control the stress distribution in the system and the overall behavior of the structure from bending dominant to stretching dominant system. We also showed the application of the structures designed using Polyhedral Graphic Statics in self-healing structural components and 3D-printed structural systems with maximized surface area and minimized mass. Another important topic was the extension of the methods of Polyhedral Graphic Statics to non-polyhedral systems using disjointed force polyhedra. In the end, advanced topics related to completeness, being, and kinematics in Polyhedral Graphic Statics were discussed, which opened the door to many further research directions in this field.
We investigate the fluid–solid interaction of suspensions of Kolmogorov-size spherical particles moving in homogeneous isotropic turbulence at a microscale Reynolds number of $Re_\lambda \approx 140$. Two volume fractions are considered, $10^{-5}$ and $10^{-3}$, and the solid-to-fluid density ratio is set to $5$ and $100$. We present a comparison between interface-resolved (PR-DNS) and one-way-coupled point-particle (PP-DNS) direct numerical simulations. We find that the modulated energy spectrum shows the classical $-5/3$ Kolmogorov scaling in the inertial range of scales and a $-4$ scaling at smaller scales, with the latter resulting from a balance between the energy injected by the particles and the viscous dissipation, in an otherwise smooth flow. An analysis of the small-scale flow topology shows that the particles mainly favour events with axial strain and vortex compression. The dynamics of the particles and their collective motion studied for PR-DNS are used to assess the validity of the PP-DNS. We find that the PP-DNS predicts fairly well both the Lagrangian and Eulerian statistics of the particle motion for the low-density case, while some discrepancies are observed for the high-density case. Also, the PP-DNS is found to underpredict the level of clustering of the suspension compared with the PR-DNS, with a larger difference for the high-density case.
This chapter introduced the geometric steps of construction to find the equilibrium for concurrent and non-concurrent systems of forces in both 2D and 3D. It showed that constructing the force polygon in 2D and the closed force polygon in 3D as a force diagram ensures that the sum of the forces in the system is zero. In addition, we learned that constructing a closed funicular polygon in 2D and a closed funicular polyhedron in 3D in the form diagram guarantees moment equilibrium in the system. We need both constructions to have a complete equilibrium. Various configurations of forces in 3D were introduced, and the process of finding the resultant by constructing the closed force polyhedron and funicular polyhedron was discussed. Ultimately, we showed how it is possible to design various hanging sculptures similar to those of Alexander Calder using geometric construction of forces and finding resultants in 2D. The design of such sculptures in 3D was pursued by subdividing the force diagram and locating equilibrating forces in the form diagram. With this introduction to equilibrium and funicular construction, we are ready to move to the next chapter, where the funicular construction for specific boundary conditions is discussed, and the principles of compression-only or tension-only structural form finding for architectural structures will be explained.
This chapter covers various topics on the design of funicular forms with an emphasis on particular features in the structural forms. It starts by introducing the topological and geometrical relationship between the form and force diagrams in 2D and 3D and describes nodal and global equilibrium in the context of both 2D and polyhedral graphic statics. It explains how to find closed polyhedral cells from a group of faces and the computational approach that could be used for this purpose. It argues the necessity of implementing computational tools to explore the realm of intricate funicular forms with pronounced design features. To give instances of how computational implementation can help in design, various design examples are introduced, and their related design topics are explained. Note that the design domain in this approach is the force diagram. Thus all these design features are explained with respect to techniques of design incorporated in the force diagram that gives the desired feature in the funicular form. In the end, the translation of the cellular to shellular systems is explained and discussed as an interesting design approach that results in a more resilient structural form by creating anticlastic curvature in three-dimensional space.
Chapter One introduces the geometric principles of equilibrium for concurrent systems of forces both in 2D and Polyhedral Graphic Statics. It starts with a simple example of a tensile or a compression-only node and explains constructing a closed force diagram for the given geometry in 2D and 3D. The chapter describes the geometrical and topological properties of a single force polygon in 2D and a polyhedron in 3D and its relationship with the static equilibrium of forces in a single node as the form diagram. In addition, the static determinacy and indeterminacy of forces are explained by the number of independent edges in the force diagram, which is referred to as the Geometric Degrees of Freedom. Furthermore, the construction of an indeterminate force polyhedron for a general node with multiple members or applied loads is discussed by explaining the Extended Gaussian Image of a polyhedron. The final examples of this chapter show how the knowledge of this chapter can be applied in the conceptual design of simple bridges with both tension and compression members.
Many problems in elastocapillary fluid mechanics involve the study of elastic structures interacting with thin fluid films in various configurations. In this work, we study the canonical problem of the steady-state configuration of a finite-length pinned and flexible elastic plate lying on the free surface of a thin film of viscous fluid. The film lies on a moving horizontal substrate that drives the flow. The competing effects of elasticity, viscosity, surface tension and fluid pressure are included in a mathematical model consisting of a third-order Landau–Levich equation for the height of the fluid film and a fifth-order Landau–Levich-like beam equation for the height of the plate coupled together by appropriate matching conditions at the downstream end of the plate. The properties of the model are explored numerically and asymptotically in appropriate limits. In particular, we demonstrate the occurrence of boundary-layer effects near the ends of the plate, which are expected to be a generic phenomenon for singularly perturbed elastocapillary problems.