Importancia de los sustratos biogénicos para el cangrejo de piedra Menippe nodifrons Stimpson, 1859 (Brachyura: Eriphioidea)

Conselho Nacional de Desenvolvimento Científico e Tecnológico (CNPq)

As origens da teoria dos invariantes na Inglaterra e o Mécanique Analytique de Lagrange (1788)

Pós-graduação em Educação Matemática - IGCE

Produção, comércio e tensões nas vilas do norte da capitania de São Paulo (1788-1808)

Coordenação de Aperfeiçoamento de Pessoal de Nível Superior (CAPES)

A presença feminina na ação educacional presbiteriana no Brasil do século XIX (1859-1899)

Conselho Nacional de Desenvolvimento Científico e Tecnológico (CNPq)

Morfologia hemipeniana de 11 espécies do gênero Micrurus Wagler, 1824 na Amazônia Brasileira, com redescrição de Micrurus filiformis (Günther, 1859) e Micrurus paraensis Cunha & Nascimento, 1973 (Serpentes, Elapidae)

O gênero Micrurus reúne serpentes de hábitos semi-fossoriais, terrestres e semiaquáticos, distribuídas desde o Sul dos Estados Unidos até o Sul da Argentina. Entre as cerca de 66 espécies atualmente válidas, 25 são registradas para a Amazônia brasileira. Com o objetivo de ampliar o conhecimento das serpentes do gênero Micrurus na Amazônia brasileira, foram levantados neste trabalho dados de lepidose, hemipênis e distribuição geográfica de 544 exemplares de 11 espécies. O presente trabalho compreende dois capítulos. O primeiro capítulo apresenta uma descrição comparativa dos hemipênis de 11 espécies de Micrurus. Baseado nos resultados obtidos nas análises dos exemplares foi elaborada diagnose, padrão de desenho e coloração, descrição e representação do hemipênis e mapa de distribuição geográfica para cada táxon. Neste capítulo são apresentadas descrições inéditas dos hemipênis de M. hemprichii ortoni e M. paraensis além de variações morfológicas até então não descritas da morfologia hemipeniana das espécies. O segundo capítulo apresenta uma descrição mais detalhada de duas espécies, M. filiformis e M. paraensis, com base na morfologia externa e do hemipênis.

Corpos-de-prova tubulares soldados e respectivo dispositivo para ensaios de fadiga sob esforços co-planares

O presente modelo de utilidade refere-se à configuração ou configurações de corpos-de-prova tubulares soldados e um dispositivo desenvolvido para induzir-lhes esforços combinados de tração e flexão a partir dos carregamentos axiais. Os corpos-de-prova são compostos por dois tubos metálicos (1, 2) aos quais são soldados dois tubos diversos (3, 4), posicionados diametralmente opostos e em diversos ângulos, preferencialmente em ângulos múltiplos de 15<198>. Refere-se ainda a um dispositivo para ensaio, ao qual são acoplados corpos-de-prova, de modo a permitir ensaios de resistência à fadiga sob esforços coplanares. Os braços do corpo-de-prova (8) são montados nos braços (9) do dispositivo. Pinos (10) são encaixados nos braços (9) e fixados.

Experimental RTM manufacturing analysis of carbon/epoxy composites for aerospace application

The success of manufacturing composite parts by liquid composite molding processes with RTM depends on tool designs, efficient heat system, a controlled injection pressure, a stabilized vacuum system, besides of a suitable study of the preform lay-up and the resin system choice. This paper reports how to assemble a RTM system in a laboratory scale by specifying heat, injection and vacuum system. The design and mold material were outlined by pointing out its advantages and disadvantages. Four different carbon fiber fabrics were used for testing the RTM system. The injection pressure was analyzed regarding fiber volume content, preform compression and permeability, showing how these factors can affect the process parameters. The glass transition temperature (Tg) around 203 ºC matched with the aimed temperature of the mold which ensured good distribution of the heat throughout the upper and lower mold length. The void volume fraction in a range of 2% confirmed the appropriate RTM system and parameters choice.

Tricot stitched carbon fiber reinforced polymer composite laminates manufactured by resin transfer molding process: C-scan and flexural analysis

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

Fatigue Behavior of Weld Repaired AISI 4130 Aeronautic Steel Used in Critical Flight Safety Structures

Since the 1950s, fatigue is the most important project and operational consideration for both civil and military aircrafts. For some aircraft models the most loaded component is one that supports the motor: the Motor Cradle. Because they are considered critical to the flight safety the aeronautic standards are extremely rigorous in manufacturing them by imposing a zero index of defects on the final weld quality (Safe Life), which is 100% inspected by Non-Destructive Testing/NDT. This study has as objective to evaluate the effects of up to four successive TIG welding repairs on the axial fatigue strength of an AISI 4130 steel. Tests were conducted on hot-rolled steel plate specimens, 0.89 mm thick, with load ratio R = 0.1, constant amplitude, at 20 Hz frequency and in room temperature, in accordance with ASTM E466 Standard. The results were related to microhardness and microstructural and geometric changes resulting from welding cycles.

Influence of shot peening on the fatigue strength of Custom 465 stainless steel for aeronautic application

This project was originated from the national aircraft industry requirements to reduce the use of coated materials with electroplated chromium or cadmium that produce waste, which is harmful to health or the environment. The selected material is a Custom 465 stainless steel used in the aeronautical field due to its high mechanical strength. Considering the load sustained by the wheel axis of the landing gear, the Custom 465 is tested in axial fatigue. The objective is to compare the behavior of the Custom 465 with plated AISI 4340 steel coated with cadmium. X-ray diffraction method was used to determine the residual stress field induced by shot peening.

O romance europeu do século XIX: uma leitura de Notre-Dame de Paris (1831) de Victor Hugo e A tale of two cities (1859) de Charles Dickens

Coordenação de Aperfeiçoamento de Pessoal de Nível Superior (CAPES)

FATIGUE IN CUSTOM 465 STAINLESS STEEL FOR AERONAUTIC APPLICATION

This project was originated from the national aircraft industry requirements to reduce the use of coated materials with electroplated chromium or cadmium that produce waste, which is harmful to health or the environment. The selected material is a Custom 465 stainless steel used in the aeronautical field due to its high mechanical strength. Considering the load sustained by the wheel axis of the landing gear, the Custom 465 was tested in axial fatigue. The objective is to compare the behavior of the Custom 465 stainless steel with plated AISI 4340 steel coated with cadmium. Fractographic analysis was conducted using scanning electron microscopy. X-ray diffraction method was used to determine the residual stress field induced by shot peening.

Revista Popular (1859-1863) e Jornal das Famílias (1863-1878): um perfil dos periódicos de Garnier

The purpose of this paper is to show some characteristics and essential information related to the Brazilian periodicals in the 19th century Revista Popular (1859-1862) and Jornal das Famílias (1863-1878), whose owner was the Frenchman Baptiste Louis Garnier. By that time the proliferation of periodicals attracts attention mainly because several of them had ephemeral existence, in opposition to Garnier’s periodicals which as a whole amount to 19 years in circulation. The research on these periodicals becomes relevant since they are well succeeded publications whose study makes possible the widening of the knowledge on social and cultural aspects of a very important period in Brazilian society.