Yes / This experimental study of forward gravure coating considers the effects of operating variables on air entrainment, ribbing instabilities and the thickness of the film formed. The data show that this coating method can yield very thin films of thickness of order of 15 - 20% at most of the equivalent cell depth of a gravure roller. Air free and non ribbed stable uniform films can however only be obtained in a narrow window of operating conditions at very low substrate capillary number (CaS ~ 0.02) equivalent to substrate speeds typically less than 20m/min. The paper draws a similarity with flow features observed with smooth forward roll coating and slide coating. It is shown that the onset of ribbing and the flux distribution between the gravure roller and the substrate at the exit of the nip obey approximately the same rules as in smooth forward roll coating, whereas the onset of air entrainment actually corresponds to a low-flow limit of coatability similar to that observed in slide coating.

Multiphase flows occurring in pipelines with a serpentine configuration is an important phenomenon, which can be encountered in heat exchangers used in a variety of industrial processes. More specifically, in many industrial units such as a large cracking furnace in a refinery, the tubes are arranged in a serpentine manner and are relatively short. As flow negotiates round the 180o bend at the ends of the tubes, the generated centrifugal force could cause flow maldistribution creating local dry spots, where no steady liquid film is formed on the adjacent straight sections of the pipe. As a result, events including coking, cracking and overheating of heat transfer surfaces may occur and lead to frequent shutdown of the facilities. Consequently, this could increase operating costs and reduce production revenue. Thus, it is desirable to know the effect that the bends exert on the flow in the straight part of the pipe. Apart from this, knowledge of the bend effects on the flows in the pipeline could also be important for the design of other pipelines for gas/liquid transport, e.g. offshore gas and oil pipelines. Quite a large number of studies have been found in the literature. The majority of them were for two-phase flow with small diameter pipes (i.d. ≤ 50 mm). However, studies with large diameter pipes (i.d. ≥ 100 mm), have increasingly been considered in recent years as problems related to large diameter vertical pipes are being encountered more and more often in industrial situations. This thesis studies the effect of 180o bends on the characteristics and development of gas-liquid two-phase flows in large diameter downward and upward pipes. The study particularly focuses on the influence of serpentine configuration on flow structure, cross-sectional void distribution and circumferential liquid film profiles and their development along the downward and upward sections. It was found that both the top and bottom bends have considerable impacts on flow behaviour, although to varying degrees. These impacts were highly dependent on the air and water flow rates. For sufficient flow rates, the bends were observed to create flow maldistribution in the adjacent straight section, due to the effects of centrifugal force. The air moved towards the inner zone of the bend and the water towards the outer zone, while a lesser quantity of water was identified on the other surfaces of the pipe. Investigation of the film thickness development in the downward and upward sections showed that, the liquid film behaviour close to the bends was significantly different from those located further away. This can be attributed to the centrifugal force of the bends. Examination of the power spectral density (PSD) along the downward and upward sections showed that, the shape of PSD located in the adjacent section to the bends, was substantially different from those located further away. Furthermore, several flow regime maps were generated which showed that, in addition to bubbly, intermittent and annular flows, unstable flows existed along the upward section, particularly for low gas and water flow rates. In this study it was found that, the lower bend was periodically blocked by the liquid and then blown through by the accumulated air. The data obtained from this study were compared with different theoretical correlations found in the existing literature. Some discrepancy between the results of the current study and those of previous published materials was noted. Updated correlations were presented which provided well results when they applied for the data obtained from the current study and previous studies.

O desenvolvimento de novos sistemas cerâmicos propicia a possibilidade de escolha do tipo de restauração que se deseje utilizar. Entretanto, os benefícios advindos deste progresso devem ser avaliados frente à possibilidade de comportamento clínico insatisfatório. Este trabalho se propõe a avaliar infra-estruturas cerâmicas quanto à influência do ajuste interno na adaptação, o desajuste vertical após a simulação da cimentação, a espessura de película nas superfícies axiais e oclusal e a ocorrência de assentamento oblíquo. Um troquel-padrão metálico com preparo para coroa total em pré-molar superior foi confeccionado e trinta troquéis de gesso foram obtidos e dividos em três grupos de dez espécimes cada. Sobre os troquéis de gesso foram confeccionadas infra-estruturas metálicas para o grupo MC, infra-estruturas cerâmicas In-Ceram Zirconia, para o grupo IZ, e Procera AllZircon, para o grupo PZ. As infra-estruturas tiveram sua posição, em relação ao troquel-padrão, mensurada durante ajuste interno e simulação da cimentação com silicone de consistência fluida (cimento-análogo). A película de cimento-análogo abaixo das infra-estruturas foi seccionada no sentido vestíbulo-lingual e mensurada nas paredes axiais e oclusal. A análise dos resultados demonstrou que: 1) o ajuste interno das infra-estruturas metalo-cerâmicas e In-Ceram Zirconia resultou em redução do desajuste vertical; 2) o desajuste vertical das infra-estruturas Procera AllZircon foi estatisticamente diferente das infra-estruturas metalo-cerâmicas e In-Ceram Zirconia; 3) a espessura de película das infra-estruturas Procera AllZircon foi significantemente maior que das infra-estruturas metalo-cerâmicas e In-Ceram Zirconia; 4) todas as infra-estruturas apresentaram assentamento oblíquo. / The development of new ceramic systems creates the possibility of choice above the type of restoration one could mean to choose. Thus, benefits from this progress must be appraised on the possibility of unsatisfactory clinical behavior. This work intends to evaluate ceramic copings to the influence of internal adjustment on adaptation, vertical misfit after cementation, film thickness of axial and occlusal surfaces and occurrence of oblique seating. A metallic superior premolar analogue with full crown preparation was yield and thirty casts were obtained and divided into three groups of ten specimens each. Metal copings were yield for group MC and ceramics copings of In-Ceram Zirconia and Procera AllZircon were yield for group IZ and group PZ, respectively. The copings had their position, in relation to the metallic analogue, measured during adjustment and cementation with light body silicon. Cement film, below the copings, was sectioned and measured at the axial and occlusal surfaces. The analysis of the results demonstrated that: 1) internal adjustment of metal and In-Ceram Zirconia copings reduced the vertical misfit; 2) vertical misfit after cementation of Procera AllZircon copings was statistically different from metal and In-Ceram Zirconia copings; 3) film thickness of Procera AllZircon copings was significantly greater than metal and In-Ceram Zirconia copings; 4) all copings presented oblique seating.

<p>Engine development is now driven by cost, performance, governmental regulations and customer demands. Several of the requirements have tribological associations. Tribological improvements which consist in lowering friction and improving wear resistance in engines, will play a major role to increase reliability and life cycle.</p><p>The components studied here are parts of the valvetrain mechanism of heavy-duty Diesel engines. The injection cam is one of the most problematic parts of the camshaft, as it is subjected to high pressures from the fuel injector. Lubrication is of significant importance in the prevention of cam failure caused by wear. However, the satisfactory lubrication of the cam and roller contact has proved to be one of the most difficult tribological design challenges to take up.</p><p>For a lubricated contact, the degree of separation between surfaces has a very strong influence on the type and amount of wear. This degree of separation is termed as specific film thickness ; its value provides a measure of the severity of asperities interaction in the lubricated contact. In this report, attention is drawn on the evaluation of oil film thickness in the cam-roller contact, in order to predict regimes of lubrication and thus to identify the probable wear zones of the injection cam. Then, confrontation with experimental results is performed(observation of worn cam surfaces). Future work to achieve is to discover the influence of the different parameters on oil film thickness, by performing a multivariate analysis. The next step will focus on modelling the wear of injection cams, and finally establishing quantified correlations between wear and specific film thickness.</p>

<p>The focus of this study is to synthesize a novel hinged polymer actuator. The linking molecule (hinge) is phenazine with interconnected dipyrrole units.</p>

Two-phase liquid-gas flow has a wide variety of applications in space, including active thermal control systems, high-power communications satellites, heat pumps and space nuclear reactors. Two-phase systems have many potential advantages over current single-phase systems due to reductions in system size, weight and power consumption. The mechanisms of pressure drop, heat transfer coefficients, void fractions, and flow regimes must be well understood under microgravity conditions in order to design reliable two-phase systems. The main objective of this present research is to develop a new mathematical model that can accurately predict the annular two-phase friction pressure drop to optimize the design of two-phase systems. The two-phase flow tests were conducted aboard the NASA KC-135 aircraft by the Interphase Transport Phenomena (ITP) group from Texas A&M University. The two-phase flow pressure drops were measured across a single transparent test section 12.7 mm ID and 1.63 m long in annular regimes under microgravity conditions during two flight campaigns. Different from previous work, this was the first time both the void fraction and the film thickness were measured under microgravity conditions. The empirical correlations for the interfacial friction factor and void fraction were developed from 57 experimental data using a linear least squares regression technique. The annular two-phase friction pressure drop can be predicted by the new mathematical model requiring only knowledge of the length and diameter of the tube, liquid and vapor mass flow rates, and properties of the working fluid. In addition, the new mathematical model was validated using Foster-Miller & ITP data collected over twelve flights aboard the KC-135 with working fluid R-12 (77 data points), Sundstrand data collected aboard the KC-135 with working fluid R-114 (43 data points) and Zhao and Rezkallah data aboard the KC-135 with working fluid water and air (43 data points). Compared with the LockhartMartinelli model, Wheeler model, Chen model and homogeneous model, the new mathematical model is the optimal model for predicting the two-phase friction pressure drop in annular regimes. The majority of the data falls within +-20% of the proposed correlation and the average error is 12%.

In this study laminar forced film condensation of vapor flowing in cross-flow direction through the annular space between two concentric cylinders was investigated numerically. To achieve this, governing equations of the vapor and the condensate flow in cross-flow direction between two concentric cylinders were developed. After obtaining the equations in integral forms by using the finite difference technique the vapor boundary layer thicknesses on the inner and outer cylinders and the condensate layer thickness was obtained as a function of the angular position on the cylinders. It was assumed that the condensation took place on the outer surface of the inner cylinder only and the outer cylinder was assumed to be insulated. The computer program developed is capable to calculate the condensate film thickness, vapor boundary layer thickness, the heat flux and the heat transfer coefficient and the interface velocity between the condensate and the vapor layer as a function of the angular position on the cylinders. Effects of changing the free stream velocity flowing in the channel, the radius of the inner cylinder, the temperature difference between the saturated vapor and the wall and the annular space between the concentric cylinders were investigated numerically by using the computer program and the results were presented graphically. Results showed that by increasing the free stream velocity of the vapor in the core, the film thickness decreased and by increasing the radius of the inner cylinder, the temperature difference between the saturated vapor and the wall and the annular space, the film thickness increased.

EDS is a tool for quantitative and qualitative analysis of the materials. In electron microscopy, the energy of the electrons determines the depth of the region where the X-rays come from. By varying the energy of the electrons, the depth of the region where the X-rays come from can be changed. If a thin film is used as a specimen, different quantitative ratios of the elements for different electron energies can be obtained. Unique thickness of a specific film on a specific substrate gives unique energy-ratio diagram so the thickness of a thin film can be calculated by analyzing the fingerprints of the energy-ratio diagram of the EDS data obtained from the film.

Abstract ¡@¡@The motion when two parting in machine into contact can combine squeeze and sliding motion. This situation does occur for example in the meshing of gear teeth and in heavily loaded rolling elements bearing etc. In this study, the experiment is used to investigate the microscopic mechanism of the oil film under the combined squeeze and sliding motion. ¡@¡@The laser optical system is employed in the starting friction tester to measure the film thickness accurately by the principle of optical interferometry. High-speed video camera with the microscope records the dynamic characteristics of lubrication in the diminutive contact region. ¡@¡@Results show that the dimple becomes deeper with increasing squeeze velocity. When sliding velocity increases, the duration of dimple becomes shorter, but when the squeeze load increases, the dimple can keep longer. Furthermore, the dimple diameter increases with increasing the curvature radius of steel ball at the same experiment condition.

<p>Measurements of film mass flow rate for annular, diabatic steam-water flow in tubes are presented. The measurements were carried out with four axial power distributions and at several axial positions at conditions typical for boiling water reactors, i.e. 7 MPa pressure and total mass flux in a range from 750 to 1750 kg/m2s. The results show that the influence of the axial power distribution on the dryout power corresponds to a consistent tendency in the film flow rate and that the film tends to zero when dryout is approached. Furthermore it is demonstrated that two selected phenomenological models of annular flow well predict the present data. A model for additional entrainment due to boiling is shown to degrade the predictions.</p>