TG studies of a composite solid rocket propellant based on HTPB-binder

Thermal decomposition kinetics of solid rocket propellants based on hydroxyl-terminated polybutadiene-HTPB binder was studied by applying the Arrhenius and Flynn-Wall-Ozawa's methods. The thermal decomposition data of the propellant samples were analyzed by thermogravimetric analysis (TG/DTG) at different heating rates in the temperature range of 300-1200 K. TG curves showed that the thermal degradation occurred in three main stages regardless of the plasticizer (DOA) raw material, the partial HTPB/IPDI binder and the total ammonium perchlorate decompositions. The kinetic parameters E-a (activation energy) and A (pre-exponential factor) and the compensation parameter (S-p) were determined. The apparent activation energies obtained from different methods showed a very good agreement.

Integrating open source codes for solid modeling and automatic mesh generation in FEM applications

The applications of the Finite Element Method (FEM) for three-dimensional domains are already well documented in the framework of Computational Electromagnetics. However, despite the power and reliability of this technique for solving partial differential equations, there are only a few examples of open source codes available and dedicated to the solid modeling and automatic constrained tetrahedralization, which are the most time consuming steps in a typical three-dimensional FEM simulation. Besides, these open source codes are usually developed separately by distinct software teams, and even under conflicting specifications. In this paper, we describe an experiment of open source code integration for solid modeling and automatic mesh generation. The integration strategy and techniques are discussed, and examples and performance results are given, specially for complicated and irregular volumes which are not simply connected. © 2011 IEEE.

Processing and characterization of ablative composites used in rocket motors

The main objective of this research work was to obtain two formulations of ablative composites. These composites are also known as ablative structural composites, for applications in atmospherically severe conditions according to the high-temperature, hot gaseous products flow generated from the burning of solid propellants. The formulations were manufactured with phenolic resin reinforced with chopped carbon fiber. The composites were obtained by the hot compression molding technique. Another purpose of this work was to conduct the physical and chemical characterization of the matrix, the reinforcements and the composites. After the characterization, a nozzle divergent of each formulation was manufactured and its performance was evaluated through the rocket motor static firing test. According to the results found in this work, it was possible to observe through the characterization of the raw materials that phenolic resins showed peculiarities in their properties that differentiate one from the other, but did not exhibit significant differences in performance as a composite material for use in ablation conditions. Both composites showed good performance for use in thermal protection, confirmed by firing static tests (rocket motor). Composites made with phenolic resin and chopped carbon fiber showed that it is a material with excellent resistance to ablation process. This composite can be used to produce nozzle parts with complex geometry or shapes and low manufacturing cost.

Caracterização de juntas soldadas em PAW e GTAW de chapas finas em aço maraging 300 submetidas a vários reparos

Pós-graduação em Engenharia Mecânica - FEG

Efeito da concentração do catalisador acetilacetonato férrico na cura de poliuretano à base de polibutadieno líquido hidroxilado (PBLH) e diisocianato de isoforona (IPDI)

Fundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)

Desempenho operacional da colheita mecanizada de cana-de-açúcar (saccharum spp.) em função da velocidade de deslocamento e rotação do motor da colhedora

Pós-graduação em Agronomia (Energia na Agricultura) - FCA

Relação entre desenvolvimento motor corporal e aquisição de habilidades orais

TEMA: a literatura aponta para a influência da postura corporal sobre as habilidades orais em crianças com desenvolvimento sensório-motor alterado. em crianças normais existem poucos estudos sobre essa relação. OBJETIVO: estudar em crianças a termo a relação entre habilidades motoras e habilidades motoras orais, desde 1 dia de vida até 24 meses de idade. MÉTODO: 42 crianças foram filmadas com 1 dia, 1 mês, 2, 3, 4, 5, 6, 9,12 e 24 meses nas posições supino, prono, sentado e em pé e durante alimentação com amamentação / mamadeira (até 5 meses), uso de colher para alimentação pastosa (3 aos 12 meses), uso de copo para água ou suco (6 aos 24 meses) e alimento sólido (6 aos 24 meses). Estabeleceram-se escores de quantificação para o desenvolvimento corporal e habilidades orais e utilizou-se o coeficiente de correlação de Pearson para o estudo estatístico, adotando-se nível de significância de 5%. RESULTADOS: os resultados do desenvolvimento motor apontaram para semelhança de dados entre supino e prono e sentado e em pé; para as habilidades orais (durante a alimentação com mamadeira/amamentação, colher, copo, mastigação) constatou-se em cada modalidade de alimentação, homogeneidade de aquisição de habilidades para lábios, língua e mandíbula. Houve associação entre habilidades motoras e orais; resultados apontam que o desenvolvimento motor (habilidades motoras) se deu antes das orais desde o 5° ao 24° mês e que as habilidades de mandíbula em copo e colher ocorreram antes das habilidades de lábios e língua. CONCLUSÃO: houve crescente aquisição de habilidades motoras e orais, variabilidade de habilidades em idades entre 3 e 24 meses e associação entre habilidades motoras e orais.

Análise dos sprays de jatos de injetores de motor foguete utilizando um sistema de processamento digital de imagens

Coordenação de Aperfeiçoamento de Pessoal de Nível Superior (CAPES)

Efeito de sistemas de irrigação localizada sobre a produção e qualidade da acerola (Malpighia spp) na região da nova alta paulista

Fundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)

Inter-relações da produtividade de cana-de-açúcar com atributos físico-químicos de um argissolo vermelho eutrófico do noroeste paulista

Coordenação de Aperfeiçoamento de Pessoal de Nível Superior (CAPES)

Enxertia de plantas de pimentão em Capsicum spp. no manejo de nema tóides de galha

Coordenação de Aperfeiçoamento de Pessoal de Nível Superior (CAPES)

Análise temporal da composição, abundância, diversidade dos Cladocera e crescimento alométrico da Daphnia spp. O. F. Müeller, 1785 na Lagoa do Camargo, lateral ao Rio Paranapanena em sua zona de desembocadura na Represa do Jurumirim

Coordenação de Aperfeiçoamento de Pessoal de Nível Superior (CAPES)

Modeling of multiple cracks in reinforced concrete members using solid finite elements with high aspect ratio

This paper presents a new technique to model interfaces by means of degenerated solid finite elements, i.e., elements with a very high aspect ratio, with the smallest dimension corresponding to the thickness of the interfaces. It is shown that, as the aspect ratio increases, the element strains also increase, approaching the kinematics of the strong discontinuity. A tensile damage constitutive relation between strains and stresses is proposed to describe the nonlinear behavior of the interfaces associated with crack opening. To represent crack propagation, couples of triangular interface elements are introduced in between all regular (bulk) elements of the original mesh. With this technique the analyses can be performed integrally in the context of the continuum mechanics and complex crack patterns involving multiple cracks can be simulated without the need of tracking algorithms. Numerical tests are performed to show the applicability of the proposed technique, studding also aspects related to mesh objectivity.

Modelagem de motor de combustão internae simulação do processo de queima de combustível

The internal combustion engine is a heat engine widely used in the automotive industry. In order to better understand its behavior many models in the literature have been proposed in the last years. The 0-D thermodynamic model is a fairly simple tool but it is very useful to understand the phenomenon of combustion inside the chamber of internal combustion engines. In the first phase of this work, an extensive literature review was made in order to get information about this kind of analysis and, after this, apply them in a model able to calculate the instantaneous temperature and pressure in one zone of the combustion chamber of a diesel engine. Therefore some considerations were made with the aim of increasing the accuracy of the model in predicting the correct behavior of the engine, adding the combined effects of heat transfer, leakage and injection. In the second phase, the goal was to study the internal flow of a three-dimensional model of an internal combustion engine. In order to achieve this goal the software Solidworks was used to create the geometries of an engine and the suite of softwares Ansys was used to create the moving mesh (ICEM CFD and CFX-Pre) and to solve the CFD problem (Ansys CFX code). The model was able to perform the air flow simulation during the four-stroke cycle of an engine: admission, compression, expansion and exhaust. The results obtained from both models were suitable and they open a new range of possibilities for future researches on the field

Projeto e análise de um sistema de ancoragem para um motor foguete a combustível líquido

This work aims the design and analysis of a thrust frame system for a liquid fuel rocket engine. The project was developed following the design requirements established by the Division of Space Propulsion of the Institute of Aeronautics and Space. The layout of the structure was developed with the aid of a software of 3D modeling and static and dynamic analysis were performed by using a finite element package. The results of the analyzes helped in defining the layout of the structure which met all design requirements. The safety factor and the mass achieved were comfortably low, which may be useful in the future because the liquid fuel rocket engine is still in development