Heating of the transmission foil separating the vacuum diodes from the laser cell in electron-beam-pumped gas lasers due to electron beam attenuation necessitates an active cooling scheme to prevent its failure under repetitively pulsed operating conditions. Attenuation of the electron beam (typically 500kV, 100kA and 100ns) produces a strong and pulsed volumetric heat source in the relatively thin (~25μm thick) stainless-steel foil causing it to fail. An experimental and numerical investigation has been conducted to study the cooling effectiveness of high-speed near-wall jets for a single stainless-steel foil strip simulating the geometry between two hibachi ribs in the Electra KrF gas laser developed by the Naval Research Laboratory. The foil is placed inside a channel with continuous gas flow simulating the circulating laser gas. Detailed studies include two jet types (planar and circular) and two injection methods (parallel and impinging) for two designs of hibachi (flat and scalloped). The planar jet flows parallel to the circulating laser gas along the entire foil span. The other configuration uses small diameter (0.8, 1.2 and 1.6 mm) circular jets positioned in two staggered rows located on the foil's two edges along the height of the foil (~30 cm). The jets are issued obliquely towards the foil. For both jet configurations, experiments are conducted at different jet velocities, impingement angles and jet-foil spacing to identify the optimal parameters to be used in the actual hibachi foil cooling. Experimental results are also compared to the predictions from CFD simulations using FLUENT®. The results of this research show that near-wall impinging circular jets can effectively cool the foil separating the vacuum diodes from the laser cell in an electron beam pumped KrF laser under prototypical pulsed (5Hz) operating conditions, thereby assuring the foil's survival, while minimizing the impact on electron beam quality and laser efficiency.

This research comprises an experimental and theoretical study on convective boiling inside tubes containing twisted-tape inserts. The demand for more compact and efficient thermal systems, in which the heat exchangers plays an important role, has led to the development and use of various heat transfer enhancement techniques. Among them twisted-tape insert as a swirl flow device is one of the most used. Twisted-tape inserts have been used for over more than one century ago as a technique of heat transfer enhancement applied to heat exchangers. However, the heat transfer augmentation comes together with pressure drop increment, impacting the pumping power and, consequently, the system efficiency. Moreover, until now it is not clear, the operational conditions under which the heat transfer coefficient augmentation by the use of twisted-tape inserts overcomes pressure drop penalty. In the present study, initially, extensive investigations of the literature concerning convective boiling inside plain tubes with and without twisted-tape inserts were performed. This literature review covers pressure drop, heat transfer coefficient and the leading frictional pressure drop gradient and heat transfer coefficient predictive methods during convective boiling inside tubes with and without twisted-tape inserts. Then, pressure drop and heat transfer coefficient results acquired in the present study were obtained in an experimental apparatus of 12.7 and 15.9 mm ID tubes during flow boiling of R134a for twisted-tape ratios of 3, 4, 9, 14 and tubes without inserts, mass velocities ranging from 75 to 200 kg/m2 s, saturation temperatures of 5 and 15°C and heat fluxes of 5 and 10 kW/m2. The experimental results were parametrically analyzed and compared against the predictive methods from literature. An analysis of the enhancement of the heat transfer coefficient and the pressure drop penalty is presented. Heat transfer coefficient increments up to 45% keeping the same pumping power and pressure drop penalty of about 35% were obtained by using twisted-tape relative to tubes without inserts. Additionally, through comparison of the present study experimental results with the predictive methods from the literature for heat transfer coefficient during two-phase flow inside tube containing twisted-tape inserts, it was verified that non of these methods predict satisfactory well the experimental results. However, a new method was develop for predicting the heat transfer coefficient during flow boiling inside tubes containing twisted-tape inserts based on the experimental results obtained in the present study. The predictive method takes into account the physical picture of the swirl flow phenomenon by including swirl flow effects promoted by the twisted-tape inserts. The proposed method predicts satisfactorily well the data obtained in the present study, predicting 89.1% of the experimental data within an error band of ± 30% and absolute mean deviation of 15.7%. / A presente pesquisa trata-se de um estudo teórico e experimental sobre a ebulição convectiva no interior de tubos com fitas retorcidas. A crescente demanda por sistemas térmicos mais compactos e eficientes, nos quais os trocadores de calor apresentam elevada relevância, tem motivado o desenvolvimento de inúmeras técnicas de intensificação de troca de calor, sendo que a utilização de fitas retorcidas é uma das técnicas mais adotadas. Fitas retorcidas são utilizadas como técnicas de intensificação de troca de calor há mais de um século. Entretanto o incremento da transferência de calor é acompanhado do aumento da perda de pressão, que por sua vez implica em aumento da potência de bombeamento, e consequentemente afeta a eficiência global do sistema. Adicionalmente, até os dias de hoje não há consenso sobre as condições operacionais em que o ganho com o incremento do coeficiente de transferência de calor é superior à perda devido ao aumento da perda de pressão. Neste estudo, inicialmente foi realizada uma extensa revisão da literatura sobre a ebulição convectiva no interior de tubos com e sem fitas retorcidas. Esta revisão aborda aspectos relacionados à perda de pressão e ao coeficiente de transferência de calor, juntamente com os métodos de previsão destes parâmetros. Foram realizados experimentos para determinação experimental de perda de pressão e coeficiente de transferência de calor, em aparato experimental contando com tubos horizontais com diâmetros internos iguais a 12,7 e 15,9 mm, para escoamento bifásico de R134a, razões de retorcimento iguais a 3, 4, 9, 14 e tubo sem fita, velocidades mássicas entre 75 e 200 kg/m²s, temperaturas de saturação iguais a 5 e 15°C, e fluxo de calor iguais a 5 e 10 kW/m². Os resultados experimentais foram analisados e comparados com estimativas segundo métodos disponíveis na literatura. Uma análise do aumento do coeficiente de transferência de calor e da perda de pressão friccional é apresentada. Foram verificados incrementos do coeficiente de transferência de calor de até 45% para a mesma potência de bombeamento, e aumento de perda de pressão de aproximadamente 35% para tubos com fitas retorcidas em relação aos tubos sem fita. Adicionalmente, através da comparação dos resultados experimentais com os métodos de previsão para coeficiente de transferência de calor, foi verificado que nenhuma metodologia apresentava previsões satisfatórias dos resultados. Portanto um novo método para previsão do coeficiente de transferência de calor durante ebulição convectiva no interior de tubos com fitas retorcidas foi desenvolvido com base nos resultados experimentais obtidos durante o presente estudo. O método proposto é função de parâmetros geométricos e do escoamento, e também de parâmetros físicos do escoamento rotacional induzido pela fita. A metodologia desenvolvida apresenta previsões satisfatórias dos resultados experimentais, prevendo 89,1% dos resultados experimentais com erro inferior a ± 30% e erro médio absoluto igual a 15,7%.

In the last few decades, augmentation of heat transfer has emerged as an important research topic. Although many promising heat transfer enhancement techniques have been proposed, such as the use of longitudinal vortex generators, few researches deal with thermal optimization. In the present work, it was conducted an optimization of delta winglet vortex generators position and angles in a fin-tube compact heat exchanger with two rows of tubes in staggered tube arrangement. Two approaches were evaluated: Response Surface Methodology (Neural Networking) and Direct Optimization. Finite-Volume based commercial software (Fluent) was used to analyze heat transfer, flow structure and pressure loss in the presence of longitudinal vortex generators (LVG). The delta winglet aspect ratio was 2 and the Reynolds numbers, based on fin pitch, were 250 and 1400. Four vortex generator parameters which impact heat exchanger performance were analyzed: LVG position in direction x-y, attack angle (θ) and roll angle (ᵩ). The present work is the first to study the influence of LVG roll angle on heat transfer enhancement. In total, eight independent LVG parameters were considered: (x₁y₁θ₁ᵩ₁) for the first tube and (x₂y₂θ₂ᵩ₂) for the second tube. Factor Analysis method (software ModeFrontier) was used to study of the influence of these LVG parameters in heat exchanger performance. The effect of each LVG parameter on heat transfer and pressure loss, expressed in terms of Colburn factor (j) and Friction factor (f), respectively, were evaluated. The optimized LVG configurations led to heat transfer enhancement rates that are much higher than reported in the literature. Direct Optimization reported better results than Response Surface Methodology for all objective functions. Important interactions were found between VG1 and VG2, which influenced the results of Colburn (j) and Friction (f) factors for each Reynolds number. Particularly, it was found that the asymmetry of the LVG, in which the VG2 parameters strongly depend on the VG1 parameters, plays a key role to enhance heat transfer. Moreover, for each Reynolds number and each objective function, there is an optimal LVG arrangement. If the objective is to mitigate pressure drop, VG1 may be suppressed because its main goal is increasing the heat transfer downstream. On the other hand, VG2 was relevant for both increase the heat transfer and decrease the pressure drop. Roll angle had a strong influence on Friction factor (f), especially for VG1 and low Reynolds number. / Por muitos anos, a intensificação da transferência de calor tem despontado como um importante tópico de pesquisa. Embora existam muitas técnicas eficazes de intensificação da transferência de calor, como o uso de geradores de vórtices, poucos trabalhos de pesquisa lidam com a otimização. Neste trabalho, foi realizada a otimização das posições e ângulos dos geradores de vórtice longitudinal (LVG) tipo meia asa delta, considerando um trocador de calor tubo-aleta compacto com duas linhas de tubos desalinhados. Duas abordagens foram empregadas: Método da Superfície de Resposta (Neural Networking) e Otimização Direta. Um software comercial (Fluent), baseado na metodologia de volumes finitos, foi empregado na análise numérica da transferência de calor, estruturas vorticais e perda de pressão no escoamento, na presença de LVG. A razão de aspecto dos geradores de vórtice foi 2 e o número de Reynolds, baseado na distância entre as aletas, foram de 250 e 1400. Foram analisados quatro parâmetros dos LVG, os quais impactam na performance do trocador de calor: a posição do LVG na direção x-y, o ângulo de ataque (θ) e o ângulo de rolamento (ᵩ). O ângulo de rolamento foi primeiramente estudado neste trabalho. No total, oito parâmetros independentes do LVG foram considerados: (x₁y₁θ₁ᵩ₁) para o primeiro tubo e (x₂y₂θ₂ᵩ₂) para o segundo tubo. O método da Análise Fatorial (software ModeFrontier) foi aplicado no estudo da influência destes parâmetros dos LVG na performance do trocador de calor. Também foi avaliado o efeito de cada um destes parâmetros na transferência de calor e perda de pressão do escoamento, expressos em termos do fator de Colburn (j) e do fator de Atrito (f), respectivamente. As configurações otimizadas dos LVG, conduziram à taxas de transferência de calor maiores do que aquelas reportadas pela literatura. A Otimização Direta mostrou resultados melhores do que através da metodologia de Superfície de Resposta para todas as funções objetivas avaliadas neste trabalho. Importantes interações foram identificadas entre VG1 e VG2, os quais influenciaram nos resultados dos fatores de Colburn (j) e Atrito (f) para cada número de Reynolds. Particularmente, foi identificado que a assimetria dos LVG desempenha um papel fundamental na intensificação da transferência de calor, onde os parâmetros de VG2 dependem fortemente dos parâmetros de VG1. Além disso, para cada número de Reynolds e para cada função objetivo, existe uma configuração ótima dos parâmetros do LVG. Se o objetivo é a redução da perda de pressão global, VG1 poderia ser suprimido da modelagem, pois a sua principal função é aumentar a transferência de calor ao longo da aleta. Por outro lado, VG2 foi relevante tanto para aumentar a transferência de calor quanto para diminuir a perda de pressão. O ângulo de rolamento teve grande influência sobre o resultado do fator de Atrito (f), especialmente para VG1 e para baixo número de Reynolds.

Developments regarding internal cooling techniques have allowed the operation of modern gas turbine engines at turbine inlet temperatures which exceed the metallurgical capability of the turbine blade. This has allowed the operation of engines at a higher thermal efficiency and lower specific fuel consumption. Modern turbine blade-cooling techniques rely on external film cooling to protect the outer surface of the blade from the hot gas path and internal cooling to remove thermal energy from the blade. Optimization of coolant performance and blade-life estimation require knowledge regarding the influence of cooling application on the blade inner and outer surface heat transfer. The following study describes a combined experimental and computational study of heat transfer augmentation near the entrance to a film-cooling hole. Steady-state heat transfer results were acquired by using a transient measurement technique in an 80 x actual rectangular channel, representing an internal cooling channel of a turbine blade. Platinum thin-film gauges were used to measure the inner surface heat transfer augmentation as a result of thermal boundary layer renewal and impingement near the entrance of a film-cooling hole. Measurements were taken at various suction ratios, extraction angles and wall temperature ratios with a main duct Reynolds number of 25×103. A numerical technique, based on the resolution of the unsteady conduction equation, using a Crank-Nicholson scheme, was used to obtain the surface heat flux from the measured surface temperature history. Computational data was generated with the use of a commercial CFD solver. / Dissertation (MEng)--University of Pretoria, 2008. / Mechanical and Aeronautical Engineering / unrestricted

In this research, an elastic cylinder that utilized vortex-induced vibration (VIV) was applied to improve convective heat transfer rates by disrupting the thermal boundary layer. Rigid and elastic cylinders were placed across a fluid channel. Vortex shedding around the cylinder led to the periodic vibration of the cylinder. As a result, the flow-structure interaction (FSI) increased the disruption of the thermal boundary layer, and therefore, improved the mixing process at the boundary. This study aims to improve convective heat transfer rate by increasing the perturbation in the fluid flow. A three-dimensional numerical model was constructed to simulate the effects of different flow channel geometries, including a channel with a stationary rigid cylinder, a channel with a elastic cylinder, a channel with two elastic cylinders of the same diameter, and a channel with two elastic cylinders of different diameters. Through the numerical simulations, the channel maximum wall temperature was found to be reduced by approximately 10% with a stationary cylinder and by around 17% when introducing an elastic cylinder in the channel compared with the channel without the cylinder. Channels with two-cylinder conditions were also studied in the current research. The additional cylinder with the same diameter in the fluid channel only reduced the surface wall temperature by 3% compared to the channel without any cylinders because the volume of the second cylinder could occupy some space, and therefore, reduce the effect of the convective heat transfer. By reducing the diameter of the second cylinder by 25% increased the effect of the convection heat transfer and reduced the maximum wall temperature by around 15%. Compared to the channel with no cylinder, the introduction of cylinders into the channel flow was found to increase the average Nusselt number by 55% with the insertion of a stationary rigid cylinder, by 85% with the insertion of an elastic cylinder, by 58% with the insertion of two cylinders of the same diameter, and by approximately 70% with the insertion of two cylinders of different diameters (the second cylinder having the smaller diameter). Furthermore, it was also found that the maximum local Nusselt number could be enhanced by around 200%-400% at the entrance of the fluid channel by using the elastic cylinders compared to the channel without cylinders.

<div>The growing need to improve the power density of compact thermal systems necessitates developing new techniques to modulate the convective heat transfer efficiently. In the present research, acoustic streaming is evaluated as a potential technology to achieve this objective. Numerical simulations using the linearized and fully non-linear Navier-Stokes equations are employed to characterize the physics underlying this process. The linearized Navier-Stokes equations accurately replicate the low-frequency flow unsteadiness, which is used to find the optimal control parameters. Local and global stability analysis tools were developed to identify the modes with a global and positive heat transfer effect.</div><div><br></div><div>High-fidelity numerical simulations are performed to evaluate the effect of the excitation at selected frequencies, directed by the linear stability analysis, on the heat and momentum transport in the flow. Results indicate that, under favorable conditions, superimposing an acoustic wave, traveling along with the flow, can <i>resonate</i> within the domain and lead to a significant heat transfer enhancement with minimal skin friction losses. Two main flow configurations are considered; at the fixed Reynolds number Re_b=3000, in the supersonic case, 10.1% heat transfer enhancement is achieved by an 8.4% skin friction increase; however, in the subsonic case, 10% enhancement in heat transfer only caused a 5.3% increase to the skin friction. The deviation between these two quantities suggests a violation of the Reynolds analogy. This study is extended to include a larger Reynolds number, namely Re_b=6000 at M_b=0.75 and a similar response is observed. The effect of excitation amplitude and frequency on the resonance, limit-cycle oscillations, heat transfer, and skin friction are also investigated here.</div><div><br></div><div>Applying acoustic waves normal to the flow in the spanwise direction disrupts the near-wall turbulent structures that are primarily responsible for heat and momentum transport near the solid boundary. Direct numerical simulations were employed to investigate this technique in a supersonic channel flow at M_b=1.5 and Re_b=3000. The external excitation is applied through a periodic body force in the spanwise direction, mimicking loudspeakers placed on both walls that are operating with a 180^o phase shift. By keeping the product of forcing amplitude A_f and pulsation period (<i>T</i>) constant, spanwise velocity perturbations are generated with a similar amplitude at different frequencies. Under this condition, spanwise pulsations at <i>T</i>=20 and <i>T</i>=10 show up to 8% reduction in Nusselt number as well as the skin friction coefficient. Excitation at higher or lower frequencies fails to achieve such high level of modulations in heat and momentum transport processes near the walls.<br> <br>In configurations involving a spatially-developing boundary layer, a computational setup that includes laminar, transitional, and turbulent regions inside the domain is considered and the impact of acoustic excitation on this flow configuration has been characterized. Large-eddy simulations with dynamic Smagorinsky sub-grid scale modeling has been implemented, due to the excessive computational cost of DNS calculations at high-Reynolds numbers. The optimal excitation frequency that resembles the mode chosen for the fully-developed case has been identified via global stability analysis. Fully non-linear simulations of the spatially-developing boundary layer subjected to the excitation at this frequency reveal an interaction between the <i>pulsations</i> and the perturbations originated from the tripping which creates a re-laminarization zone traveling downstream. Such technique can locally enhance or reduce the heat transfer along the walls.<br></div>

<p>With the extreme increases in power density of electronic devices, the contact thermal resistance imposed at interfaces between mating solids becomes a major challenge in thermal management. This contact thermal resistance is mainly caused by micro-scale surface asperities (roughness) and wavy profile of surface (nonflatness) which severely reduce the contact area available for heat conduction. High contact pressures (1~100 MPa) can be used to deform the surface asperities to increase contact area. Besides, a variety of conventional thermal interface materials (TIM), such as greases and pastes, are used to improve the contact thermal conductance by filling the remaining air gaps. However, there are still some applications where such TIMs are disallowed for reworkability concerns. For example, heat must be transferred across dry interfaces to a heat sink in pluggable opto-electronic transceivers which needs to repeatedly slide into / out of contact with the heat sink. Dry contact and low contact pressures are required for this sliding application.</p> <p>This dissertation presents a metallized micro-spring array as a surface coating to enhance dry contact thermal conductance under ultra-low interfacial contact pressure. The shape of the micro-springs is designed to be mechanically compliant to achieve conformal contact between nonflat surfaces. The polymer scaffolds of the micro-structured TIMs are fabricated by using a custom projection micro-stereolithography (μSL) system. By applying the projection scheme, this method is more cost-effective and high-throughput than other 3D micro-fabrication methods using a scanning scheme. The thermal conductance of polymer micro-springs is further enhanced by metallization using plating and surface polishing on their top surfaces. The measured mechanical compliance of TIMs indicates that they can deform ~10s μm under ~10s kPa contact pressures over their footprint area, which is large enough to accommodate most of surface nonflatness of electronic packages. The measured thermal resistances of the TIM at different fabrication stages confirms the enhanced thermal conductance by applying metallization and surface polishing. Thermal resistances of the TIMs are compared to direct metal-to-metal contact thermal resistance for flat and nonflat mating surfaces, which confirms that the TIM outperforms direct contact. A thin layer of soft polymer is coated on the top surfaces of the TIMs to accommodate surface roughness that has a smaller spatial period than the micro-springs. For rough surfaces, the polymer-coated TIM has reduced thermal resistance which is comparable to a benchmark case where the top surfaces of the TIM are glued to the mating surface. A polymer base is designed under the micro-spring array which can provide the advantages for handling as a standalone material or integration convenience, at the toll of an increased insertion resistance. Through-holes are designed in the base layer and coated with thermally conductive metal after metallization to enhance thermal conductance of the base layer; a thin layer of epoxy is applied between the base layer and the working surface to reduce contact thermal resistance exposed on the base layer. Cycling tests are conducted on the TIMs; the results show good early-stage reliability of the TIM under normal pressure, sliding contact, and temperature cycles. The TIM is thermally demonstrated on a pluggable application, namely, a CFP4 module, which shows enhanced thermal conductance by applying the TIM. </p> To further enhance the potential mechanical compliance of microstructured surfaces, a stable double curved beam structure with near-zero stiffness composed of intrinsic negative and positive stiffness elastic elements is designed and fabricated by introducing residual stresses. Stiffness measurements shows that the positive-stiffness single curved beam, which is the same as the top beam in the double curved beam, is stiffer than the double curved beam, which confirms the negative stiffness of the bottom beam in the double curved beam. Layered near zero-stiffness materials made of these structures are built to demonstrate the scalability of the zero-stiffness zone.

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No description available.

<p>  </p> <p>Acoustic streaming is a phenomenon which occurs when acoustic excitations interact with a fluid (stationary or non-stationary). Exploitation of this phenomenon has the potential to open doors to new methods of flow control through the enhancement or diminishment of the present flow instabilities. A particular use of acoustic streaming shown by previous numerical studies is the enhancement of heat transfer in violation of the Reynold’s Analogy within a small range of Mach numbers and frequencies of periodic excitation. The focus of this thesis is to experimentally assess the usage of a Rossiter cavity in generating periodic acoustic excitations and its effects on the shear stress and heat transfer. </p> <p>In the present research, two large models are tested using a blow-down facility. The models are made of aluminum and Teflon and were developed to ensure optical access for infrared thermography. The geometries are tested at Mach number ranging from 0.373 to 0. 866. The target Mach number-frequency pair where significant heat transfer enhancement is a free stream Mach number at the cavity, Mc, of 0.75 and the frequency, fc, of 7.5 kHz. The cavity is tuned using the Rossiter equation with Rossiter constants k = 0.66 and y = 0.25. The heat transfer and skin friction enhancement are measured immediately upstream and downstream of the cavity and compared to the previous numerical studies.</p> <p>When testing the Teflon model with an ambient back pressure and 11 lb/s mass flow, a frequency of 7.8 kHz was generated by the cavity. For the aluminum model tested at a high vacuum and 3 lb/s mass flow, frequencies near 7, 10, and 20 kHz were generated by the cavity with 10 and 20 kHz appearing most often. High speed schlieren imaging was used to confirm the flow structures being generated in the flow. There was good agreement with the Rossiter modes at lower Mach numbers and moderate agreement at transonic Mach numbers. A correlation is presented which defines a band of Mach number-Reynolds number pairs which present with a discontinuous frequency behavior during operation of the wind tunnel. Measurable effects on both skin friction and heat transfer between tests with comparable operating conditions to a reference were observed and are presented.</p>