Optimization of nanotube electrode geometry in a liquid crystal media from wavefront aberrations

This paper presents experimental optimization of number and geometry of nanotube electrodes in a liquid crystal media from wavefront aberrations for realizing nanophotonic devices. The refractive-index gradient profiles from different nanotube geometries-arrays of one, three, four, and five-were studied along with wavefront aberrations using Zernike polynomials. The optimizations help the device to make application in the areas of voltage reconfigurable microlens arrays, high-resolution displays, wavefront sensors, holograms, and phase modulators. © 2012 Optical Society of America.

Nonsmooth geometry and collapse of flexible structures under smooth loads

While static equilibria of flexible strings subject to various load types (gravity, hydrostatic pressure, Newtonian wind) is well understood textbook material, the combinations of the very same loads can give rise to complex spatial behaviour at the core of which is the unilateral material constraint prohibiting compressive loads. While the effects of such constraints have been explored in optimisation problems involving straight cables, the geometric complexity of physical configurations has not yet been addressed. Here we show that flexible strings subject to combined smooth loads may not have smooth solutions in certain ranges of the load ratios. This non-smooth phenomenon is closely related to the collapse geometry of inflated tents. After proving the nonexistence of smooth solutions for a broad family of loadings we identify two alternative, critical geometries immediately preceding the collapse. We verify these analytical results by dynamical simulation of flexible chains as well as with simple table-top experiments with an inflated membrane.

Geometry and interaction of structures in homogeneous isotropic turbulence

A strategy to extract turbulence structures from direct numerical simulation (DNS) data is described along with a systematic analysis of geometry and spatial distribution of the educed structures. A DNS dataset of decaying homogeneous isotropic turbulence at Reynolds number Reλ = 141 is considered. A bandpass filtering procedure is shown to be effective in extracting enstrophy and dissipation structures with their smallest scales matching the filter width, L. The geometry of these educed structures is characterized and classified through the use of two non-dimensional quantities, planarity' and filamentarity', obtained using the Minkowski functionals. The planarity increases gradually by a small amount as L is decreased, and its narrow variation suggests a nearly circular cross-section for the educed structures. The filamentarity increases significantly as L decreases demonstrating that the educed structures become progressively more tubular. An analysis of the preferential alignment between the filtered strain and vorticity fields reveals that vortical structures of a given scale L are most likely to align with the largest extensional strain at a scale 3-5 times larger than L. This is consistent with the classical energy cascade picture, in which vortices of a given scale are stretched by and absorb energy from structures of a somewhat larger scale. The spatial distribution of the educed structures shows that the enstrophy structures at the 5η scale (where η is the Kolmogorov scale) are more concentrated near the ones that are 3-5 times larger, which gives further support to the classical picture. Finally, it is shown by analysing the volume fraction of the educed enstrophy structures that there is a tendency for them to cluster around a larger structure or clusters of larger structures. Copyright © 2012 Cambridge University Press.

Self-consistent geometry in the computation of the vibrational spectra of molecules

An exact and general approach to study molecular vibrations is provided by the Watson Hamiltonian. Within this framework, it is customary to omit the contribution of the terms with the vibrational angular momentum and the Watson term, especially for the study of large systems. We discover that this omission leads to results which depend on the choice of the reference structure. The self-consistent solution proposed here yields a geometry that coincides with the quantum averaged geometry of the Watson Hamiltonian and appears to be a promising way for the computation of the vibrational spectra of strongly anharmonic systems.

Design of a thick-walled screen for flow equalization in microstructured reactors

A systematic computational fluid dynamics (CFD) approach has been applied to design the geometry of the channels of a three-dimensional (thick-walled) screen comprising upstream and downstream sets of elongated channels positioned at an angle of 90 degrees with respect to each other. Such a geometry of the thick-wall screen can effectively drop the ratio of the maximum flow velocity to mean flow velocity below 1.005 in a downstream microstructured reactor at low Reynolds numbers. In this approach the problem of flow equalization reduces to that of flow equalization in the first and second downstream channels of the thick-walled screen. In turn, this requires flow equalization in the corresponding cross-sections of the upstream channels. The validity of the proposed design method was assessed through a case study. The effect of different design parameters on the flow non-uniformity in the downstream channels has been established. The design equation is proposed to calculate the optimum values of the screen parameters. The CFD results on flow distribution were experimentally validated by Laser Doppler Anemometry measurements in the range of Reynolds numbers from 6 to 113. The measured flow non-uniformity in the separate reactor channels was below 2%.

A numerical study of trailing edge geometry for low inertia automotive mixed flow turbines

Abstract. Mixed flow turbines can offer improvements over typical radial turbines used in automotive turbochargers, with respect to transient performance and low velocity ratio efficiency. Turbine rotor mass dominates the rotating inertia of the turbocharger’s rotating assembly, and any reductions of mass in the outer radii of the wheel, including the rotor back-disk, can significantly reduce this inertia and improve the acceleration of the assembly. Off-design, low velocity ratio conditions are typified by highly tangential flow at the rotor inlet and a non-zero inlet blade angle is desirable for such operating conditions. This is achievable in a Mixed Flow Turbine without increasing bending stresses within the rotor blade, which is beneficial in high speed and high inlet temperature turbine designs.
This study considers the meridional geometry of Mixed Flow Turbines using a multi-disciplinary study to assess both the structural and aerodynamic performance of each rotor, incorporating both CFD and FEA. Variations of rotor trailing edge were investigated at different operating conditions representing both on- and off-design operation within the constraints of existing hardware geometries. In all cases, the performance is benchmarked against an existing state-of-the-art radial turbocharger turbine with consideration of rotor inertia and its benefit for engine transient performance. The results indicate the influence of these parameters and this report details their benefits with respect to turbocharging a downsized, automotive engine.

A numerical study of automotive turbocharger mixed flow turbine inlet geometry for off design performance

Mixed flow turbines represent a potential solution to the increasing requirement for high pressure, low velocity ratio operation in turbocharger applications. While literature exists for the use of these turbines at such operating conditions, there is a lack of detailed design guidance for defining the basic geometry of the turbine, in particular, the cone angle – the angle at which the inlet of the mixed flow turbine is inclined to the axis. This investigates the effect and interaction of such mixed flow turbine design parameters.
Computational Fluids Dynamics was initially used to investigate the performance of a modern radial turbine to create a baseline for subsequent mixed flow designs. Existing experimental data was used to validate this model.
Using the CFD model, a number of mixed flow turbine designs were investigated. These included studies varying the cone angle and the associated inlet blade angle.
The results of this analysis provide insight into the performance of a mixed flow turbine with respect to cone and inlet blade angle.

Hydraulics of stepped chutes: experimental-numerical-theoretical study

O estudo de escoamentos turbulentos em descarregadores em degraus tem sido um desafio para os investigadores. A macro-rugosidade do leito, a ondulação da superfície livre, a intermitência da localização da secção inicial de entrada de ar e o escoamento bi-fásico a jusante da secção inicial de entrada de ar fazem com que a caracterização do escoamento deslizante sobre turbilhões em descarregadores em degraus não seja simples. Actualmente, é possível combinar técnicas de medição fiáveis com simulações numéricas e análise teórica. Nesta dissertação, o estudo experimental baseia-se em resultados experimentais obtidos em duas instalações experimentais: a instalação A, do Laboratório Nacional de Engenharia Civil (LNEC), dotada de um descarregador em degraus com declive de 1V:0.75H e a instalação B, do Instituto Superior Técnico (IST), dotada de um descarregador em degraus com declive de 1V:2H. Uma sonda de ar, um tubo de Pitot modificado e vários hidrómetros permitiram o estudo do escoamento deslizante sobre turbilhões mono- e bifásico ao longo do descarregador em degraus da instalação A. Na bacia de dissipação de energia, a observação visual do escoamento foi auxiliada pelas leituras efectuadas em tomadas de pressão localizadas na soleira da bacia e pelas leituras da altura do escoamento efectuadas em réguas graduadas localizadas nas paredes da bacia. Na instalação B foram utilizados um tubo de Pitot e vários hidrómetros para estudar a região não arejada do escoamento deslizante sobre turbilhões no descarregador em degraus. O estudo numérico é baseado em simulações numéricas da região não arejada do escoamento deslizante sobre turbilhões sobre descarregadores em degraus com o código comercial de CFD FLOW-3D® de modo a reproduzir as condições ensaiadas experimentalmente. As simulações beneficiaram da técnica de blocos múltiplos (multi-block) num sistema de coordenadas cartesianas, da determinação da superfície livre pelo método TruVOF e da utilização de dois modelos de turbulência: os modelos k- e RNG k-. Por último, o estudo teórico consistiu em desenvolver um modelo simplificado 1D para determinar as características hidráulicas principais do trecho não arejado do escoamento deslizante sobre turbilhões em descarregadores em degraus. O modelo foi desenvolvido a partir das equações de Navier-Stokes, conjuntamente com resultados experimentais e numéricos. Os resultados apresentados nesta dissertação contribuem para o conhecimento do escoamento deslizante sobre turbilhões em descarregadores em degraus, nomeadamente na região não arejada, na secção inicial de entrada de ar e na região arejada. A hidráulica dos dissipadores de energia a jusante de descarregadores em degraus, em particular das bacias tipo III do USBR, é também objecto de estudo. Em relação à região não arejada do escoamento em descarregadores com declive acentuado, e com base em resultados experimentais e numéricos, são propostas expressões para estimar o desenvolvimento da altura equivalente de água, da espessura da camada limite, da concentração média de ar, do coeficiente de energia cinética, da dissipação de energia, do factor de resistência e do coeficiente n da fórmula de Manning. São ainda propostas expressões adimensionais para a energia cinética turbulenta e sua dissipação. Para declives moderados, são propostas expressões para estimar o desenvolvimento da altura equivalente de água, do coeficiente de energia cinética e da energia específica residual. São ainda apresentados valores do expoente 1/N da expressão adimensional da distribuição de velocidades, quer para descarregadores com declive acentuado quer com declive moderado. Em conformidade com outros estudos centrados em escoamentos de parede e com derivações teóricas, para a região não arejada do escoamento em descarregadores em degraus de acentuado declive, observa-se que o factor de resistência depende da macro-rugosidade criada pelos degraus e da geometria da secção transversal e que o coeficiente n da fórmula de Manning aumenta com a rugosidade. A descrição estatística da turbulência do escoamento é igualmente explorada, contribuindo para o conhecimento da estrutura do escoamento. Observou-se que para números de Reynolds rugoso não superiores a 6.8x104 a energia cinética turbulência e a sua dissipação cumprem leis de semelhança. Estas expressões adimensionais estão de acordo com os resultados obtidos por outros autores para escoamentos completamente desenvolvidos em canais abertos e no escoamento em rios com leito de gravilha. Em acréscimo, a taxa de dissipação de energia, quer para descarregadores de declive acentuado quer de moderado declive, é baixa. Por último, observa-se que os valores da média temporal da concentração de ar entre 0 e 1 medidos na região não arejada do escoamento dizem respeito não só ao ar capturado entre ondas de água, na zona de ondulação da superfície livre, mas também ao ar emulsionado no escoamento, i.e., sob a forma de bolhas de ar, quando perto da secção média inicial de entrada de ar, devido à diferença entre localizações instantânea e média temporal. Foram revistas metodologias e fórmulas para estimar a localização da secção inicial de entrada de ar e apresentadas expressões para estimar a concentração média de ar e a altura equivalente de água nessa secção. Relativamente à região de escoamento arejado em descarregadores em degraus com declive acentuado, os resultados experimentais apresentados nesta dissertação permitiram estimar a influência da definição da superfície livre nos parâmetros hidráulicos da região do escoamento arejado e estimar a máxima elevação do escoamento nesta região do escoamento. Com base nos resultados experimentais obtidos na bacia de dissipação de energia do tipo III do USBR localizada a jusante do descarregador em degraus da instalação A, observou-se que os perfis da altura piezométrica e da altura do escoamento tendem a seguir o perfil recomendado pelo USBR para bacias tipo III. A excepção ocorre à entrada da bacia, onde as alturas piezométricas apresentadas nesta dissertação excedem largamente as apresentadas pelo USBR. É ainda observado que, tal como entre as bacias tipo I e tipo III do USBR, o ressalto hidráulico estabiliza muito mais rapidamente numa bacia tipo III a jusante de um descarregador em degraus do que uma bacia tipo I a jusante do mesmo descarregador em degraus. Finalmente, observa-se que os blocos de amortecimento a colocar no descarregador não têm influência visível nos resultados da altura piezométrica nem da altura do escoamento ao longo da bacia. Relativamente às simulações numéricas do escoamento não arejado, a proximidade entre resultados experimentais e numéricos permite validar o modelo teórico e a integração numérica usados no FLOW-3D®. As simulações desenvolvidas também mostraram que o modelo de turbulência k- permite representar as características do escoamento não arejado em descarregadores em degraus, uma vez que não foram observadas diferenças significativas entre as simulações com este modelo e com o modelo RNG k-. Finalmente, observou-se que o modelo de entrada de ar usado no FLOW-3D® é válido para estimar a localização da secção inicial de entrada de ar. Por último, a proximidade entre os resultados obtidos da aplicação do modelo teórico desenvolvido no âmbito desta dissertação e os resultados experimentais indica que as hipóteses e simplificações consideradas no desenvolvimento do modelo são adequadas.

A theoretical study on modelling the respiratory tract with ladder networks by means of intrinsic fractal geometry

Fractional order modeling of biological systems has received significant interest in the research community. Since the fractal geometry is characterized by a recurrent structure, the self-similar branching arrangement of the airways makes the respiratory system an ideal candidate for the application of fractional calculus theory. To demonstrate the link between the recurrence of the respiratory tree and the appearance of a fractional-order model, we develop an anatomically consistent representation of the respiratory system. This model is capable of simulating the mechanical properties of the lungs and we compare the model output with in vivo measurements of the respiratory input impedance collected in 20 healthy subjects. This paper provides further proof of the underlying fractal geometry of the human lungs, and the consequent appearance of constant-phase behavior in the total respiratory impedance.

A case of four-coordinate silver(I) adopting a high energy planar geometry. Experiment and theory

The ligands PhL and MeL are obtained by condensing 2-formylpyridine with benzil dihydrazone and diacetyl dihydrazone, respectively, in 2: 1 molar proportion. With silver( I), PhL yields a double-stranded dinuclear cationic helicate 1 in which the metal is tetrahedral but MeL gives a cationic one-dimensional polymeric complex 2 where silver( I) is distorted square planar and the ligand backbone is nearly planar. In both complexes, metal: ligand ratio is 1: 1. Ab initio calculations on the ligands at the HF/6-31+G* level reveal that while PhL strongly prefers a helical conformation, MeL has a natural inclination to remain in a planar conformation. Density functional theory calculations on model silver( I) complexes show that formation of the linear polymer in the case of MeL is also an important factor in imposing the planar geometry of Ag(I) in 2.

Facile strategies for the synthesis and crystallization of linear trinuclear nickel(II)-Schiff base, complexes with carboxylate bridges: Tuning of coordination geometry and magnetic properties

Three new linear trinuclear nickel(II) complexes, [Ni-3(salpen)(2)(OAc)(2)(H2O)(2)]center dot 4H(2)O (1) (OAc = acetate, CH3COO-), [Ni-3(salpen)(2)(OBz)(2)] (2) (OBz=benzoate, PhCOO-) and [Ni-3(salpen)(2)(OCn)(2)(CH3CN)(2)] (4) (OCn = cinnamate, PhCH=CHCOO-), H(2)salpen = tetradentate ligand, N,N'-bis(salicylidene)-1,3-pentanediamine have been synthesized and characterized structurally and magnetically. The choice of solvent for growing single crystal was made by inspecting the morphology of the initially obtained solids with the help of SEM study. The magnetic properties of a closely related complex, [Ni-3(salpen)(2)(OPh)(2)(EtOH)] (3) (OPh = phenyl acetate, PhCH2COO-) whose structure and solution properties have been reported recently, has also been studied here. The structural analyses reveal that both phenoxo and carboxylate bridging are present in all the complexes and the three Ni(II) atoms remain in linear disposition. Although the Schiff base ligand and the syn-syn bridging bidentate mode of the carboxylate group remain the same in complexes 1-4, the change of alkyl/aryl group of the carboxylates brings about systematic variations between six- and five-coordination in the geometry of the terminal Ni(II) centres of the trinuclear units. The steric demand as well as hydrophobic nature of the alkyl/aryl group of the carboxylate is found to play a crucial role in the tuning of the geometry. Variable-temperature (2-300 K) magnetic susceptibility measurements show that complexes 1-4 are antiferromagnetically coupled (J = -3.2(1), -4.6(1). -3.2(1) and -2.8(1) cm(-1) in 1-4, respectively). Calculations of the zero-field splitting parameter indicate that the values of D for complexes 1-4 are in the high range (D = +9.1(2), +14.2(2), +9.8(2) and +8.6(1) cm(-1) for 1-4, respectively). The highest D value of +14.2(2) and +9.8(2) cm(-1) for complexes 2 and 3, respectively, are consistent with the pentacoordinated geometry of the two terminal nickel(II) ions in 2 and one terminal nickel(II) ion in 3. (C) 2009 Elsevier Ltd. All rights reserved.

Perspex machine VIII: axioms of transreal arithmetic

Transreal arithmetic is a total arithmetic that contains real arithmetic, but which has no arithmetical exceptions. It allows the specification of the Universal Perspex Machine which unifies geometry with the Turing Machine. Here we axiomatise the algebraic structure of transreal arithmetic so that it provides a total arithmetic on any appropriate set of numbers. This opens up the possibility of specifying a version of floating-point arithmetic that does not have any arithmetical exceptions and in which every number is a first-class citizen. We find that literal numbers in the axioms are distinct. In other words, the axiomatisation does not require special axioms to force non-triviality. It follows that transreal arithmetic must be defined on a set of numbers that contains{-8,-1,0,1,8,&pphi;} as a proper subset. We note that the axioms have been shown to be consistent by machine proof.

Understanding the Effect of Adsorption Geometry over Substrate Selectivity in the Surface-Enhanced Raman Scattering Spectra of Simazine and Atrazine

This paper studies the selectivity of Well-defined Au and Ag nanostructures as substrates for the SERS, (surface-enhanced Raman scattering) detection of simazine (6-chloro-N,N`-diethyl-1,3,5-triazine-2,4-diamine) and atrazine (6-chloro-N-ethyl-N`-isopropyl-1,3,5-triazine-2,4-diamine). Our data showed that simazine and atrazine displayed similar SERS spectra when the Au was employed as substrate. Conversely, distinct SERS signatures were obtained upon the utilization of Ag substrates. Density functional theory (DFT) calculations and vibrational assignments suggested that, while simazine and atrazine adsorbed on Au via the N3 position of the triazine ring, simazine adsorbed on Ag via N3 and atrazine via N5. The results presented herein demonstrated that the adsorption geometry of analyte molecules can play a central role over substrate selectivity in SERS, which is particularly important in applications involving ultrasensitive analysis of mixtures containing structurally similar molecules.

Boundary identification criteria and geometry analysis of Al 7050 stretch zone from elevation profiles

This article describes the development of a method for analysis of the shape of the stretch zone surface based on parallax measurement theory and using digital image processing techniques. Accurate criteria for the definition of the boundaries of the stretch zone are established from profiles of fracture surfaces obtained from crack tip opening displacement tests on Al-7050 alloy samples. The elevation profiles behavior analysis is based on stretch zone width and height parameters. It is concluded that the geometry of the stretch zone profiles under plane strain conditions can be described by a semi-parabolic relationship. (C) Elsevier B.V., 1999. All rights reserved.

Mathematical aspects of Feynman integrals

In the present dissertation we consider Feynman integrals in the framework of dimensional regularization. As all such integrals can be expressed in terms of scalar integrals, we focus on this latter kind of integrals in their Feynman parametric representation and study their mathematical properties, partially applying graph theory, algebraic geometry and number theory. The three main topics are the graph theoretic properties of the Symanzik polynomials, the termination of the sector decomposition algorithm of Binoth and Heinrich and the arithmetic nature of the Laurent coefficients of Feynman integrals.rnrnThe integrand of an arbitrary dimensionally regularised, scalar Feynman integral can be expressed in terms of the two well-known Symanzik polynomials. We give a detailed review on the graph theoretic properties of these polynomials. Due to the matrix-tree-theorem the first of these polynomials can be constructed from the determinant of a minor of the generic Laplacian matrix of a graph. By use of a generalization of this theorem, the all-minors-matrix-tree theorem, we derive a new relation which furthermore relates the second Symanzik polynomial to the Laplacian matrix of a graph.rnrnStarting from the Feynman parametric parameterization, the sector decomposition algorithm of Binoth and Heinrich serves for the numerical evaluation of the Laurent coefficients of an arbitrary Feynman integral in the Euclidean momentum region. This widely used algorithm contains an iterated step, consisting of an appropriate decomposition of the domain of integration and the deformation of the resulting pieces. This procedure leads to a disentanglement of the overlapping singularities of the integral. By giving a counter-example we exhibit the problem, that this iterative step of the algorithm does not terminate for every possible case. We solve this problem by presenting an appropriate extension of the algorithm, which is guaranteed to terminate. This is achieved by mapping the iterative step to an abstract combinatorial problem, known as Hironaka's polyhedra game. We present a publicly available implementation of the improved algorithm. Furthermore we explain the relationship of the sector decomposition method with the resolution of singularities of a variety, given by a sequence of blow-ups, in algebraic geometry.rnrnMotivated by the connection between Feynman integrals and topics of algebraic geometry we consider the set of periods as defined by Kontsevich and Zagier. This special set of numbers contains the set of multiple zeta values and certain values of polylogarithms, which in turn are known to be present in results for Laurent coefficients of certain dimensionally regularized Feynman integrals. By use of the extended sector decomposition algorithm we prove a theorem which implies, that the Laurent coefficients of an arbitrary Feynman integral are periods if the masses and kinematical invariants take values in the Euclidean momentum region. The statement is formulated for an even more general class of integrals, allowing for an arbitrary number of polynomials in the integrand.