4,904 research outputs found

    Robust multi-fidelity design of a micro re-entry unmanned space vehicle

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    This article addresses the preliminary robust design of a small-scale re-entry unmanned space vehicle by means of a hybrid optimization technique. The approach, developed in this article, closely couples an evolutionary multi-objective algorithm with a direct transcription method for optimal control problems. The evolutionary part handles the shape parameters of the vehicle and the uncertain objective functions, while the direct transcription method generates an optimal control profile for the re-entry trajectory. Uncertainties on the aerodynamic forces and characteristics of the thermal protection material are incorporated into the vehicle model, and a Monte-Carlo sampling procedure is used to compute relevant statistical characteristics of the maximum heat flux and internal temperature. Then, the hybrid algorithm searches for geometries that minimize the mean value of the maximum heat flux, the mean value of the maximum internal temperature, and the weighted sum of their variance: the evolutionary part handles the shape parameters of the vehicle and the uncertain functions, while the direct transcription method generates the optimal control profile for the re-entry trajectory of each individual of the population. During the optimization process, artificial neural networks are utilized to approximate the aerodynamic forces required by the optimal control solver. The artificial neural networks are trained and updated by means of a multi-fidelity approach: initially a low-fidelity analytical model, fitted on a waverider type of vehicle, is used to train the neural networks, and through the evolution a mix of analytical and computational fluid dynamic, high-fidelity computations are used to update it. The data obtained by the high-fidelity model progressively become the main source of updates for the neural networks till, near the end of the optimization process, the influence of the data obtained by the analytical model is practically nullified. On the basis of preliminary results, the adopted technique is able to predict achievable performance of the small spacecraft and the requirements in terms of thermal protection materials

    Estimação de vazão em bacias hidrogrÑficas do Sul do Espírito Santo usando o SWAT

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    O aumento da atividade econΓ΄mica e do nΓΊmero de habitantes no mundo, juntamente com o uso nΓ£o sustentΓ‘vel dos recursos hΓ­dricos, os despejos de efluentes sem tratamento no ambiente e o manejo inadequado das bacias hidrogrΓ‘ficas, tΓͺm contribuΓ­do para diminuição da disponibilidade de Γ‘gua no planeta. Apesar de ser um recurso natural renovΓ‘vel, a Γ‘gua que retorna da atmosfera nΓ£o ocorre de maneira uniformemente distribuΓ­da, nem no espaΓ§o geogrΓ‘fico, nem no tempo, tornando a sua boa gestΓ£o essencial para diminuição das consequΓͺncias desastrosas dos eventos extremos de cheia e de escassez. Mas, uma gestΓ£o exitosa requer, alΓ©m de profissionais qualificados, o uso de ferramentas para suporte Γ  tomada de decisΓ£o. Neste contexto, a utilização de modelos hidrolΓ³gicos pode auxiliar no planejamento e avaliação de prΓ‘ticas conservacionistas de solo e Γ‘gua e de manejo de bacias hidrogrΓ‘ficas. Do exposto, o presente estudo teve o objetivo de avaliar a aplicabilidade do SWAT para a estimação de vazΓ΅es em bacias hidrogrΓ‘ficas no sul do Estado do EspΓ­rito Santo. Foram estudadas: a microbacia do cΓ³rrego Jaqueira (MBJ), com aproximadamente 22,6 ha, e a sub-bacia do rio Itapemirim, Γ  montante da estação fluviomΓ©trica de Rive (BIMR), com aproximadamente 2.237 kmΒ². Devido ao alto nΓΊmero de falhas e ao curto perΓ­odo de monitoramento hidrolΓ³gico, nΓ£o foi possΓ­vel calibrar e verificar a aplicabilidade do modelo para a MBJ. Para a BIMR, na anΓ‘lise das vazΓ΅es mΓ©dias, estimou-se 45,5 mΒ³ s-1 antes da calibração, e 32,6 mΒ³ s-1 apΓ³s a calibração, muito prΓ³xima da vazΓ£o mΓ©dia monitorada de 36,9 mΒ³ s-1. Para o perΓ­odo de validação, a vazΓ£o mΓ©dia monitorada foi 22% maior (45,0 mΒ³ s-1), enquanto a estimada foi de 33,9 mΒ³ s-1, permanecendo prΓ³xima da vazΓ£o mΓ©dia estimada calibrada. Em anΓ‘lise grΓ‘fica, observou-se que, antes da calibração, as vazΓ΅es mΓ­nimas estimadas ficaram abaixo das observadas, porΓ©m as vazΓ΅es de pico eram superestimadas. ApΓ³s a calibração, as vazΓ΅es mΓ­nimas tiveram melhores correlaçáes, enquanto as vazΓ΅es de pico foram subestimadas. Na anΓ‘lise dos Γ­ndices estatΓ­sticos, o RΒ² passou de 0,74 para 0,76 apΓ³s a calibração, mas foi reduzido para 0,63 no perΓ­odo de validação. Para o coeficiente de Nash Sufcliffe, houve uma melhora significativa do valor apΓ³s a calibração, passando de -0,38 para 0,75, permanecendo com um valor aceitΓ‘vel de 0,57 no perΓ­odo de validação. O SWAT foi capaz de simular vazΓ΅es em bacias hidrogrΓ‘ficas do Sul do EspΓ­rito Santo, desde que nΓ£o houvesse muitas falhas nos dados monitorados, sendo capaz inclusive de simular dados de outros perΓ­odos para os quais os parΓ’metros nΓ£o foram ajustados

    Characterization of ply mixing rules for non-symmetric forms of fully orthotropic laminates

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    Stacking sequence listings are presented for fully orthotropic angle-ply laminates, with up to 21 plies, together with rules for mixing these sequences to form laminates containing any number of plies. The mixing rules are demonstrated through an abridged set of sequences, which are characterized in terms of angle- and cross-ply sub-sequence symmetries. The abridged set of sequences is derived from a new definitive list that supersedes previously published listings. Stacking sequences are presented together with dimensionless parameters from which the bending stiffness terms are readily calculated and an assessment of the bending stiffness efficiency made for angle- and cross-ply sub-sequences. Expressions relating the dimensionless parameters to the well-known lamination parameters are also given, together with graphical representations of feasible domains for all sub-sequence symmetries contained in the definitive list. Feasible domains for extensionally isotropic and fully isotropic laminates are also presented as important sub-sets of fully orthotropic laminates. Finally, examples are given for tapered laminates with fully orthotropic properties, derived from compatible sequences in the definite list

    Clustering data by inhomogeneous chaotic map lattices

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    A new approach to clustering, based on the physical properties of inhomogeneous coupled chaotic maps, is presented. A chaotic map is assigned to each data-point and short range couplings are introduced. The stationary regime of the system corresponds to a macroscopic attractor independent of the initial conditions. The mutual information between couples of maps serves to partition the data set in clusters, without prior assumptions about the structure of the underlying distribution of the data. Experiments on simulated and real data sets show the effectiveness of the proposed algorithm.Comment: 8 pages, 6 figures. Revised version accepted for publication on Physical Review Letter

    Stacking sequences for extensionally isotropic, fully isotropic and quasi-homogeneous orthotropic laminates

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    Stacking sequence listings are presented for fully uncoupled Extensionally Isotropic (EILs), Fully Isotropic (FILs) and Quasi-Homogeneous Orthotropic (QHOLs) angle-ply Laminates, with up to 21 plies. All are sub-sets of a definitive list of Fully Orthotropic Laminates (FOLs), containing generally non-symmetric stacking sequences that are characterized in terms of angle- and cross-ply sub-sequence symmetries. Dimensionless parameters are given for each stacking sequence, from which the ABD matrix is readily derived. Expressions relating these dimensionless parameters to the well-known lamination parameters are also given, together with graphical representations of the feasible domains for Pi/3 and Pi/4 EILs and angle-ply QHOLs containing two and three ply orientations. The feasible domain for Pi/3 FILs is represented graphically by a single point, whereas the domain for angle-ply QHOLs containing four ply orientations is represented by a single stacking sequence

    On composite laminates with extensional anisotropy

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    The definite list of extensionally (membrane) anisotropic composite laminates with up to 21 plies is presented. The listings comprise of individual stacking sequences, which are characterized in terms of angle- and cross-ply sub-sequence relationships as well as the blend-ratio of unbalanced angle-plies. Dimensionless parameters, including lamination parameters, are provided, from which the extensional and bending stiffness terms are readily calculated and an assessment of the bending stiffness efficiency made for angle- and cross-ply sub-sequences. Comparisons are made between the structural response of extensionally-anisotropic laminates and laminates with both extensional- and bending-anisotropy; Initial- and post-buckling responses are considered at the panel level together with the static response of a complete wing-box structure
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