Aerospace research for next-generation travel increasingly focuses on the use of advanced composites to reduce weight and cost while retaining strength. One subset of materials with great potential is based on the combination of resin matrix and glass-fiber reinforcement. This research explores the application of a candidate nanopaper coating with a given composite. Prior research applied a set of given heat fluxes to the top surface of the composite for a set of given periods of time, and subsequently performed a 3-point flexural test to determine the elastic modulus for both the coated and uncoated composite for all of the combinations of heat flux and time. A finite element (FE) model is developed using the ANSYS general purpose finite element analysis (FEA) software that models the degradation in strength/stiffness properties based on heating condition and with the goal of predicting cracking using the element death feature in ANSYS. This thesis describes the prior research suggesting both the need for and novelty of this model, and the procedures used to form the model. The loading conditions of the 3-point flexural test are replicated, and four measures of accuracy are developed based on the force versus displacement curve of the test and the FE model. It is envisioned that continuum-level models developed as a part of these research be applied for design of next-generation space components These measurements are used to verify the FE model, and this model is then employed to extrapolate beyond the context of experimental conditions.

Presented in this work are the results of twelve flexural tests conducted on small-scale coupons to establish the load-deflection behavior of UNS S32003 (ATI 2003®) hot-rolled duplex stainless steel flat plates. All specimens were tested as simply supported beams loaded at the midspan. Test specimens had nominal width and thickness of 1 in. and 0.25 in., respectively. Four different span lengths of 4 in., 6 in., 9 in., and 12 in. were investigated. Analysis of the results showed that the non-linear deflection behavior can be estimated reasonably well by adopting the conventional deflection equation pertaining to an assumed linear elastic material, but after replacing the modulus of elasticity with a secant modulus corresponding to the maximum tension strain resulting from the applied load.

Made available in DSpace on 2014-06-11T19:22:18Z (GMT). No. of bitstreams: 0 Previous issue date: 2007-02-18Bitstream added on 2014-06-13T18:07:52Z : No. of bitstreams: 1 verao_gb_me_sjrp.pdf: 363983 bytes, checksum: c59e477b48d1d71a3199f377018eead3 (MD5) / Coordenação de Aperfeiçoamento de Pessoal de Nível Superior (CAPES) / O objetivo deste trabalho é estudar problemas de valor de contorno do tipo {ÿ + f(t) =0 y(0)=0˙ y(1)= ky(η), (1) onde η ∈ (0, 1), k ∈ R e f ∈C([0, 1],R). Para antingirmos nosso objetivo usamosas funções de Green G(t,s)que nos permitem escrever a solução do problema(1)na seguinte forma: w(t)= ∫ 1 0 G(t,s)f(s)ds. Usando esta solução, investigamos através do ponto fixo de Schauder a solvabilidade do problema não linear { y + f(t,y)=0 y(0)=0˙ y(1)= ky(η). / The main goal of this work is study the following boundary value problems {ÿ + f(t) = 0 =0 y(0)=0˙ y(1)= ky(η), (1), where η ∈ (0, 1), k ∈ R e f ∈C([0, 1],R). To achieve our goal we use the Green's function G(t,s) which allow us to write the solution of the problem (2) in the form: w(t)= ∫ 1 0 G(t,s)f(s)ds. Using this solution and the Schauder point theory, also we study the solvability of a nonlinear problem { y + f(t,y)=0 y(0)=0˙ y(1)= ky(η).

This thesis aimed at the development of a fibre optic strain sensor-based damage detection and evaluation system (FODDAS) based on the composite beams. EFPI strain sensors were used with their integrity being assessed. Their performance, either bonded on the surfaces or embedded was examined extensively. They were shown to be adequate and reliable for strain measurements. Through-the-width damages were simulated by artificially-embedded delaminations, which were located at several through-the-thickness locations, each with two different sizes. The overall design considerations were guided by ply stresses and strains which were estimated by using the modified classical lamination theory (CLT). Considerable efforts were devoted to assessing the through-the-thickness mechanical behaviours of the beams containing optical fibres in three-point bending and short beam shear (SBS). They involved various optical fibre orientations with respect to 00 plies / longitudinal axis and at various through-the-thickness locations, each with different number of optical fibres. The understanding of these behaviours paved the way for the evaluation of the beam-based FODDAS. Smart preconditioned beams were subjected to the quasi -static loads whose magnitudes and locations were required to be well controlled. The viability and effectiveness of the beam-based FODDAS was evaluated in terms of strength and strain obtained by the embedded sensor as well as the surface-bonded strain gauges via the cross comparison of ten cases. For the strength, each beam was incrementally loaded up to the ultimate failure either in three-point bending or SBS. After each increment, the beam was unloaded and inspected for damage. For the given locations of EFPI-SS and artificial delamination as well as the sizes of the latter, it was found that the embedded EFPI-SSs were capable of picking up the stiffness degradation when the 10- mm as well as the 20-mm delamination was located at the 29-30 ply interface in the tensile region of a 32-ply quasi-isotropic carbon/epoxy smart composite beam. It was speculated from single tests results that the propagation of the embedded delamination of the sufficient size was able not only to be detected but also to be monitored by the sensors.

In order to elucidate the effects of NPY directly on bone tissue, two different doses of NPY (NPY dose 1= 1X10-5 M and NPY dose 2 = 1X 10&amp / #65533 / 6 M) and NPY dose 2 plus its inhibitor were applied together with hyaluronic acid (HA) into the intramedullary area of right tibia of Wistar rats. HA alone was administered as the control group. On three time points, day one, week one and week two after administration, the tibiae were collected and stored at &amp / #65533 / 20oC for analysis. Evaluation was performed via conventional radiography, dual energy X-ray absorbtiometry (DEXA), quantitative computerized tomography (QCT), three point bending test (TPB) and histology techniques. QCT was used to assess both atomic content and density of both medulla and cortex of tibiae. From DEXA results, it was observed that inhibition of NPY causes an increase in the bone mass from first day to second week. This phenomena was also observed in histology results so that new bone formation in the inhibitor administered bone was encountered at week two. In both medulla and cortex areas&amp / #65533 / atomic content, an increase in average effective atomic number was displayed after administration of NPY plus NPY inhibitor throughout two weeks. In addition, density of medulla of tibiae measured by QCT also revealed an increase in bone mass when inhibitor is applied throughout two weeks. As a result, overall evaluation of data obtained from DEXA, QCT and histological analysis revealed that NPY inhibits bone formation or have a pro-osteoclastic effect / inversely HA displayed osteogenic effect.

Orientador: German Jesus Lozada Cruz / Banca: Luiz Augusto Fernandes de Oliveira / Banca: José Marcio Machado / Resumo: O objetivo deste trabalho é estudar problemas de valor de contorno do tipo {ÿ + f(t) =0 y(0)=0˙ y(1)= ky(η), (1) onde η ∈ (0, 1), k ∈ R e f ∈C([0, 1],R). Para antingirmos nosso objetivo usamosas funções de Green G(t,s)que nos permitem escrever a solução do problema(1)na seguinte forma: w(t)= ∫ 1 0 G(t,s)f(s)ds. Usando esta solução, investigamos através do ponto fixo de Schauder a solvabilidade do problema não linear { y + f(t,y)=0 y(0)=0˙ y(1)= ky(η). / Abstract: The main goal of this work is study the following boundary value problems {ÿ + f(t) = 0 =0 y(0)=0˙ y(1)= ky(η), (1), where η ∈ (0, 1), k ∈ R e f ∈C([0, 1],R). To achieve our goal we use the Green's function G(t,s) which allow us to write the solution of the problem (2) in the form: w(t)= ∫ 1 0 G(t,s)f(s)ds. Using this solution and the Schauder point theory, also we study the solvability of a nonlinear problem { y + f(t,y)=0 y(0)=0˙ y(1)= ky(η). / Mestre

This study investigates the effect of strain rate on fracture properties of Ferritic-Pearlitic Ductile Iron. A series of dynamic three point bending tests, with various load application rates, are conducted on Charpy V-notch specimens, in room temperature and approximately -18 °C. The tests are performed in a custom-made fixture and during the tests, force and displacement data are recorded. A XFEM (Extended Finite Element Method) model of the test setup has been established and material data from the tests are used as input to the model. The test results show a strong dependency of the strain rate regarding the force needed for crack initiation. Moreover, it can be concluded that low temperature makes the material very brittle, even at low load application rates.

Orientador: Germán Jesus Lozada Cruz / Banca: Marco Aparecido Queiroz Duarte / Banca: Juliana Conceição Precioso Pereira / Resumo: O objetivo desse trabalho é estudar problemas de valor de contorno com três pontos lineares e não ineares, também conhecidos como problemas não Isto é feito, usando as funções de Green, usadas para resolver problemas de valor de contorno com dois pontos. / Abstract: The aim of this work is to study boundary value problems with three points also known as non-classical problems. This is done using the Green's functions, which are used to solve two-point boundary value problems. / Mestre

The diploma thesis deals with the issue of force effects in the three-point hitch links in the multi-body environment depending on the forces ejected to the plow during the plowing. Through simulations, force responses under the tractor wheels are also identified for various conditions. The work is also analyzed for the impact of the upper link attachment relative to the tractor output parameters.

Syfte Syftet med föreliggande studie var att undersöka böjhållfastheten hos IPS e.max CAD före och efter termocykling med 10 000 respektive 15 000 cykler. Material och metod Trettio provkroppar framställdes från fem stycken IPS e.max CAD LT-block. Provkropparna var indelade i två testgrupper (GT10 och GT15), och en kontrollgrupp (GK), á 10 provkroppar i varje. Provkropparna utformades enligt måtten L 17,9 ± 0,03 mm x B 2,5 ± 0,03 mm x H 2,5 ± 0,03 mm. Samtliga provkroppar kristalliserades och grupp GK förvarades i rumstemperatur, resterande två grupper, GT10 och GT15 termocyklades i 10 000 respektive 15 000 cykler.Därefter utfördes ett trepunkts böjhållfasthetstest. Resultaten analyserades med One-way ANOVA, Tukey’s test med signifikansnivån α= 0,05 i statistikprogrammet SPSS. Resultat Resultaten visade att det inte fanns någon signifikant skillnad mellan grupp GK och GT10 (p>0,05) respektive mellan grupp GT10 och GT15 (p>0,05). Grupp GT15 hade högst medelvärde (516 MPa) och grupp GK hade lägst medelvärde (450 MPa). Signifikant skillnad fanns mellan grupp GK och GT15 (p<0,05). Grupp GT15 hade en signifikant högre böjhållfasthet (~470-637 MPa) jämfört med grupp GK (~406-494 MPa). Slutsats Inom föreliggande studies begränsningar kan följande slutsatser dras: Termocykling med 10 000 cykler påverkar inte böjhållfastheten, däremot ger ökat antal cykler (15 000) högre böjhållfasthet. / Purpose  The purpose of the present study was to investigate the flexural strength of IPS e.max CAD beforeand after thermal cycling with 10,000 and 15,000 cycles, respectively.  Material and method  Thirty specimens were prepared from five IPS e.max CAD LT blocks, divided into two test groups (GT10 and GT15), and one control group (group GK) (n=10). The specimens were designed with the dimensions L 17.9 ± 0,03 mm x W 2.5 ± 0,03 mm x H 2.5 ± 0,03 mm. All specimens were crystallized and group GK was kept in room temperature, the remaining two groups, GT10 and GT15 were thermocycled with 10,000 and 15,000 cycles respectively. A three-point flexural strength test was performed. The results were analyzed with One-way ANOVA, Tukey's test with a significance level α = 0.05 in the statistical program SPSS.  Results  The results showed that there was no significant difference between groups GK and GT10 (p> 0.05), and between groups GT10 and GT15 (p> 0.05). It was also observed that group GT15 had the highest average (516 MPa) and group GK had the lowest average (450 MPa). There was a significant difference between groups GK and GT15 (p <0.05). Group GT15 had a significantly higher flexural strength (~ 470-637 MPa) compared to group GK (~406-494 MPa).  Conclusion  Within the limitations of the present study, the following conclusions can be drawn:Thermal cycling comprising 10,000 cycles do not affect the flexural strength, however, increasing the number of cycles (15,000) will give higher flexural strength.