Experimental and Numerical Investigation of Evaporative Spray Cooling for a 45 Degree Bend Near a Gas Turbine Exhaust

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Total Pages : 292 pages
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Book Synopsis Experimental and Numerical Investigation of Evaporative Spray Cooling for a 45 Degree Bend Near a Gas Turbine Exhaust by : Grant Armitage

Download or read book Experimental and Numerical Investigation of Evaporative Spray Cooling for a 45 Degree Bend Near a Gas Turbine Exhaust written by Grant Armitage and published by . This book was released on 2013 with total page 292 pages. Available in PDF, EPUB and Kindle. Book excerpt: The research performed in this work investigated evaporative spray cooling systems using water near a 45 degree bends in gas turbine exhaust piping systems. Both experimental data and numerical data were generated with the goal of evaluating the ability of Fluent 6.3.26 to predict the performance of these systems for the purpose of design using only modest computational resources. Three cases were investigated in this research: single phase exhaust flow with no water injection, injecting water before the bend and injecting water after the bend. Various probes were used to measure dry bulb temperature, total pressure and water mass flux of the two phase flow at the exit of the pipe. Seven hole probes and pitot static probes were used to measure single phase flow properties. Numerical simulations were performed using mass flow boundary conditions which were generated from experimental results. A turbulence model was selected for the simulations based on comparisons of single phase simulations with experimental data and convergence ability. Using Fluent's discrete phase model, different wall boundary conditions for the discrete phase were used in order to find the model which would best match the evaporation rates of the experimental data. Mass flux values through the exit plane of the pipe were found to be the most reliable of all the two phase data collected. Results from numerical simulations revealed the shortcomings of the available discrete phase wall boundary conditions to accurately predict the interaction of the liquid phase with the wall. Experimental results for both cases showed extensive areas of the wall which had liquid film layers running down the length of the pipe. Simulations resulted in particles either failing to impact the wall and create a liquid film, or creating a liquid film which was much smaller than the film present in experimental results. This led to 8% and 15% discrepancy in evaporation amounts between numerical and experimental results for water injection upstream and downstream of the bend respectively. Under-prediction of areas wetted with a wall film in the simulations also led to gross over predictions of wall temperature in numerical results.

An Experimental and Numerical Investigation of Evaporative Spray Cooling for a 45 Degree Bend Near a Gas Turbine Exhaust

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Book Synopsis An Experimental and Numerical Investigation of Evaporative Spray Cooling for a 45 Degree Bend Near a Gas Turbine Exhaust by : Grant Armitage

Download or read book An Experimental and Numerical Investigation of Evaporative Spray Cooling for a 45 Degree Bend Near a Gas Turbine Exhaust written by Grant Armitage and published by . This book was released on 2014 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Experimental and Computational Analysis of Evaporative Spray Cooling for Gas Turbine Exhaust Ejectors

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Total Pages : 346 pages
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Book Synopsis Experimental and Computational Analysis of Evaporative Spray Cooling for Gas Turbine Exhaust Ejectors by : Nathon Begg

Download or read book Experimental and Computational Analysis of Evaporative Spray Cooling for Gas Turbine Exhaust Ejectors written by Nathon Begg and published by . This book was released on 2011 with total page 346 pages. Available in PDF, EPUB and Kindle. Book excerpt: This research studied the effects of evaporative spray cooling on air-air ejector performance. Experimental data was collected for the purpose of validating computational simulations. This was done by modifying an existing air-air ejector to accommodate four spray flow nozzles which were used to atomize cooling water. The only parameter that was varied throughout the study was the mass flow rate of cooling water. One single phase (air) case and four spray flow cases where performed and analyzed. The purpose of the single phase experiment was to have a baseline for the air-air ejector performance and isolate the sources of experimental error contributed by spray flow. Three specialized multiphase flow instruments were designed and fabricated by the author to measure, gas phase temperatures, spray mass flow rates, and mixture total pressures. A computational study was performed using the collected experimental data for inlet continuous phase and spray mass flow as boundary conditions for equivalent simulations. A temperature gradient modified turbulence model was written by the author to better predict the mixing rates found experimentally which was used for the duration of this research. Secondary droplet breakup was modeled by the author using empirical correlations following preliminary simulations recognizing the deficiencies of commercially available breakup models. Comparison of experimental and computational cases produced mixed results. It was found that the experimental gas temperature instrument performed poorly for the local droplet fluxes encountered during testing. The spray sampling probe showed more promising results with two integrated mass flows agreeing within 6% of computational simulations. The total pressure probe solved the issue of pressure port clogging, but measurements were representative of mixture density which made an inferred velocity calculation difficult. It was found that evaporation of spray flow before the nozzle exit plane caused a reduction in dynamic pressure and a reduction in back pressure. A full scale simulation was performed to determine the effects of scaling on evaporative spray cooling performance. It was found that for the geometrically similar full scale model, the total droplet surface area and particle residence times scaled up with the model which increased cooling performance.

Experimental Investigation of External Water-spray Cooling in a Turbojet Engine Utilizing Several Injection Configurations Including Orifices in the Rotor-blade Bases

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Total Pages : 30 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Experimental Investigation of External Water-spray Cooling in a Turbojet Engine Utilizing Several Injection Configurations Including Orifices in the Rotor-blade Bases by : Roy A. McKinnon

Download or read book Experimental Investigation of External Water-spray Cooling in a Turbojet Engine Utilizing Several Injection Configurations Including Orifices in the Rotor-blade Bases written by Roy A. McKinnon and published by . This book was released on 1955 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Fluid Property Effects on Spray Cooling

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ISBN 13 :
Total Pages : 144 pages
Book Rating : 4.:/5 (89 download)

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Book Synopsis Fluid Property Effects on Spray Cooling by : Andrea C. Ashwood

Download or read book Fluid Property Effects on Spray Cooling written by Andrea C. Ashwood and published by . This book was released on 2007 with total page 144 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Experimental and Numerical Studies of Mist Cooling with Thin Evaporating Subcooled Liquid Films

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Total Pages : pages
Book Rating : 4.:/5 (71 download)

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Book Synopsis Experimental and Numerical Studies of Mist Cooling with Thin Evaporating Subcooled Liquid Films by : Vladimir Novak

Download or read book Experimental and Numerical Studies of Mist Cooling with Thin Evaporating Subcooled Liquid Films written by Vladimir Novak and published by . This book was released on 2006 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental and numerical investigation has been conducted to examine steady, internal, nozzle-generated, gas/liquid mist cooling in vertical channels with ultra-thin, evaporating subcooled liquid films. Interest in this research has been motivated by the need for a highly efficient cooling mechanism in high-power lasers for inertial fusion reactor applications. The aim is to quantify the effects of various operating and design parameters, viz. liquid atomization nozzle design (i.e. spray geometry, droplet size distribution, etc.), heat flux, liquid mass fraction, film thickness, carrier gas velocity, temperature, and humidity, injected liquid temperature, gas/liquid combinations, channel geometry, length, and wettability, and flow direction, on mist cooling effectiveness. A fully-instrumented experimental test facility has been designed and constructed. The facility includes three cylindrical and two rectangular electrically-heated test sections with different unheated entry lengths. Water is used as the mist liquid with air, or helium, as the carrier gas. Three types of mist generating nozzles with significantly different spray characteristics are used. Numerous experiments have been conducted; local heat transfer coefficients along the channels are obtained for a wide range of operating conditions. The data indicate that mist cooling can increase the heat transfer coefficient by more than an order of magnitude compared to forced convection using only the carrier gas. The data obtained in this investigation will allow designers of mist-cooled high heat flux engineering systems to predict their performance over a wide range of design and operating parameters. Comparison has been made between the data and predictions of a modified version of the KIVA-3V code, a mechanistic, three-dimensional computer program for internal, transient, dispersed two-phase flow applications. Good agreement has been obtained for downward mist flow at moderate heat fluxes; at high heat fluxes, the code underpredicts the local heat transfer coefficients and does not predict the onset of film rupture. For upward mist flow, the code underpredicts the local heat transfer coefficients and, contrary to experimental observations, predicts early dryout at the test section exit.

An Experimental and Numerical Study of Heat Transfer Augmentation Near the Entrance to a Film Cooling Hole

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ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (956 download)

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Book Synopsis An Experimental and Numerical Study of Heat Transfer Augmentation Near the Entrance to a Film Cooling Hole by : Gerard Scheepers

Download or read book An Experimental and Numerical Study of Heat Transfer Augmentation Near the Entrance to a Film Cooling Hole written by Gerard Scheepers and published by . This book was released on 2013 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.

Experimental and Numerical Conjugate Investigation of the Blowing-ratio Influence on the Showerhead Cooling Efficiency

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ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (137 download)

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Book Synopsis Experimental and Numerical Conjugate Investigation of the Blowing-ratio Influence on the Showerhead Cooling Efficiency by : Dieter E. Bohn

Download or read book Experimental and Numerical Conjugate Investigation of the Blowing-ratio Influence on the Showerhead Cooling Efficiency written by Dieter E. Bohn and published by . This book was released on 1998 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: Presented at the International Gas Turbine & Aeroengine Congress & Exhibition, Stockholm, Sweden, June 2 - June 5, 1998.

An Experimental Investigation of the Non-evaporative Spray Cooling Process for Cooling High Temperature Air Streams

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ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (717 download)

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Book Synopsis An Experimental Investigation of the Non-evaporative Spray Cooling Process for Cooling High Temperature Air Streams by : Marion John Balcerzak

Download or read book An Experimental Investigation of the Non-evaporative Spray Cooling Process for Cooling High Temperature Air Streams written by Marion John Balcerzak and published by . This book was released on 1958 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Experimental Testing and Numerical Modeling of Spray Cooling Under Terrestrial Gravity Conditions

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ISBN 13 :
Total Pages : 116 pages
Book Rating : 4.:/5 (614 download)

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Book Synopsis Experimental Testing and Numerical Modeling of Spray Cooling Under Terrestrial Gravity Conditions by : Kerri Michelle Baysinger

Download or read book Experimental Testing and Numerical Modeling of Spray Cooling Under Terrestrial Gravity Conditions written by Kerri Michelle Baysinger and published by . This book was released on 2005-01-01 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt: Baseline tests were performed for a spray cooling system using subcooled fluid under terrestrial gravity conditions, and a steady state numerical model of the glass heater pedestal assembly was built using ANSYS finite element software. A parametric study was performed to study the effects of volumetric flow rate, heat transfer rate, and orientation with respect to gravity on the experimental system. The numerical model data was compared with the experimental data in order to determine the spray heat transfer coefficient along the top of the heated surface. For a volumetric flow range gal/hr and a heat load range of W, the estimated spray heat transfer coefficient was on the order of W/(m2-K), regardless of heater orientation. In addition, the heat lost due to conduction in the upward-facing heater pedestal was estimated using both experimental and numerical results, and was found to be 1.0 greater or less than (percent of heat loss due to conduction in glass heater pedestal assembly) greater or less than 2.5%.

Experimental and numerical conjugate flow and heat transfer investigation of the influence of density ratio and blowing ratio on the film-cooling efficiency of a first stage.., ASME 99-GT-199

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ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (137 download)

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Book Synopsis Experimental and numerical conjugate flow and heat transfer investigation of the influence of density ratio and blowing ratio on the film-cooling efficiency of a first stage.., ASME 99-GT-199 by : Dieter E. Bohn

Download or read book Experimental and numerical conjugate flow and heat transfer investigation of the influence of density ratio and blowing ratio on the film-cooling efficiency of a first stage.., ASME 99-GT-199 written by Dieter E. Bohn and published by . This book was released on 1999 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: Presented at the International Gas Turbine & Aeroengine Congress & Exhibition, Indianapolis, Indiana, June 7-10, 1999.

Experimental Investigation of Water Spray Cooling Characteristics of a Solid Heated Surface

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ISBN 13 :
Total Pages : 212 pages
Book Rating : 4.:/5 (385 download)

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Book Synopsis Experimental Investigation of Water Spray Cooling Characteristics of a Solid Heated Surface by : Rainer F. Ponzel

Download or read book Experimental Investigation of Water Spray Cooling Characteristics of a Solid Heated Surface written by Rainer F. Ponzel and published by . This book was released on 1997 with total page 212 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Two-Phase Spray Cooling with Water/2-Propanol Binary Mixtures for High Heat Flux Focal Source

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Total Pages : 73 pages
Book Rating : 4.:/5 (126 download)

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Book Synopsis Two-Phase Spray Cooling with Water/2-Propanol Binary Mixtures for High Heat Flux Focal Source by : Sai Sujith Obuladinne

Download or read book Two-Phase Spray Cooling with Water/2-Propanol Binary Mixtures for High Heat Flux Focal Source written by Sai Sujith Obuladinne and published by . This book was released on 2016 with total page 73 pages. Available in PDF, EPUB and Kindle. Book excerpt: Two-phase spray cooling has been an emerging thermal management technique offering high heat transfer coefficients and critical heat flux levels, near-uniform surface temperatures, and efficient coolant usage that enables to design of compact and lightweight systems. Due to these capabilities, spray cooling is a promising approach for high heat flux applications in computing, power electronics, and optics. Two-phase spray cooling inherently depends on saturation temperature-pressure relationships of the working fluid to take advantage of high heat transfer rates associated with liquid-vapor phase change. When a certain application requires strict temperature and/or pressure conditions, thermo-physical properties of the working fluid play a critical role in attaining proper efficiency, reliability, or packaging structure. However, some of the commonly used single-component working fluids have relatively poor properties and heat transfer performance. For example, water is the best coolant in terms of properties, yet in certain applications where the system operates at low temperature ambient, it cannot be implemented due to freezing risk. The common solution for this problem is to use the antifreeze mixtures (binary mixtures of water and alcohol) to reduce the freezing point. In such cases, utilizing binary mixtures to tune working fluid properties becomes an alternative approach. This study has two main objectives; (1) to experimentally investigate the two-phase spray cooling performance of water/2-propanol binary mixture, and (2) to numerically investigate the performance of an advanced heat spreader featuring high and directional thermal conductivity materials for high heat flux focal sources. The first part of the study involves experimental characterization of heat transfer performance. Tests are conducted on a small-scale, closed loop spray cooling system featuring a pressure atomized spray nozzle. The test section, made of copper, measures 10 mm x 10 mm x 2 mm with a plain, smooth surface. A cylindrical copper block, with a matching size square protrusion attached onto the back side of the test section, generates heat using cartridge heaters and simulates high heat flux source. Embedded thermocouples are used to determine the spray surface temperature. The working fluid, water/alcohol mixture, has various concentration levels of 2-propanol by mass fraction 0.0 (pure water), 0.25, 0.50, 0.879 (azeotrope) and 1.0 (pure alcohol)), representing both non-azeotropic and azeotropic cases. Spray cooling tests are performed with a constant flow rate of 5.6 ml/cm2.s at subcooled temperatures (̃20oC) and atmospheric pressure. Experimental procedure involves controlling the heat flux in increasing steps, and recording the corresponding steady-state temperatures to obtain cooling curves in the form of surface superheat vs. heat flux. The second part of the study investigates an advanced heat spreader design for thermal management of a high heat flux focal source. The heat spreader comprises of three layers: a copper layer that interfaces with the heat source, a high and directional thermal conductivity material (such as CVD diamond and Pyrolytic graphite) layer, and another copper layer that is exposed to two-phase spray cooling. The analysis applies various heat fluxes on the heat source side and the experimentally obtained heat transfer coefficients on the spray side of the spreader design to determine the temperature and heat flux distributions, and examine the potential capabilities of this configuration.

Experimental and Numerical Investigations on Aero-thermal Interaction of Cooling Air Ejected from Multiple Cooling Holes

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Total Pages : 110 pages
Book Rating : 4.:/5 (949 download)

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Book Synopsis Experimental and Numerical Investigations on Aero-thermal Interaction of Cooling Air Ejected from Multiple Cooling Holes by :

Download or read book Experimental and Numerical Investigations on Aero-thermal Interaction of Cooling Air Ejected from Multiple Cooling Holes written by and published by . This book was released on 2013 with total page 110 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Numerical Study of Louver Cooling Scheme on Gas Turbine Airfoils

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Total Pages : 0 pages
Book Rating : 4.:/5 (462 download)

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Book Synopsis Numerical Study of Louver Cooling Scheme on Gas Turbine Airfoils by : Xuezhi Zhang

Download or read book Numerical Study of Louver Cooling Scheme on Gas Turbine Airfoils written by Xuezhi Zhang and published by . This book was released on 2008 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This work presents the performance of a louver film-cooling scheme under different operating conditions. The louver cooling scheme consists of a bend by which the coolant going through the flow passage is redirected from vertical to horizontal direction before being injected into the mainstream through an expanded exit. Not only is the momentum of the coolant converted to the mainstream direction, but it is also reduced by the expanded exit before injection. The impingement of the coolant on the blade surface inside the bend also enables further cooling on the targeted surface. The louver cooling scheme was tested under a variety of conditions, from a flat plate to airfoils, from low speed incompressible flows to transonic flows, from a stationary airfoil to a rotating airfoil, and from the leading edge to the middle of an airfoil. Unsteady analysis using a DES (Detached Eddy Simulation) model was also carried out to evaluate its ability to accurately simulate film cooling by comparing with steady state analysis. In general, the louver cooling scheme has been proved to provide enhanced cooling protection to the targeted surface in comparison with other cooling schemes in all conditions tested. At low speed incompressible flow conditions, a higher blowing ratio led to a higher cooling effectiveness. At transonic flow conditions, a moderately higher blowing ratio also proved helpful with a higher cooling effectiveness. Very high blowing ratios, however, proved to be detrimental to the cooling performance since strong detached shock wave structures due to high blowing ratios caused boundary layer separation, rendering the coolant virtually ineffective. The rotation of blade was found to have a significant impact on the level of cooling effectiveness at the leading edge of an airfoil. With regard to the cooling performance, blowing ratio was the dominant factor at low rotational speeds and the rotational speed was the dominant factor at high blowing ratios for circular holes. For the louver scheme as jet liftoff was avoided, effectiveness increased with rotating speed. Results also showed that, unsteady analysis was not significantly more accurate than steady analysis. The unsteady analysis did capture the coolant lateral spreading better, with a high cost of computing, however. Results in this work show that shock waves encountered on transonic airfoils had a significant impact on film cooling effectiveness on any shaped holes. Therefore, experimental data obtained under low speed test should be used with great caution in real design of turbine blade cooling. There are fundamental differences in film cooling between at the leading edge and elsewhere on an airfoil in that a slight incidence shifting due to turbine rotating speed may cause a sudden decrease in cooling effectiveness level at high blowing ratios for circular hole. This could lead to a catastrophic failure if the blade is already in a weak and stressed state. Using of shaped holes with expanded exits may prevent this from happening.

Numerical and Experimental Study on Pin-fin Based Cooling Structure for Gas Turbine Application

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Total Pages : pages
Book Rating : 4.:/5 (16 download)

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Book Synopsis Numerical and Experimental Study on Pin-fin Based Cooling Structure for Gas Turbine Application by : Shan Huang

Download or read book Numerical and Experimental Study on Pin-fin Based Cooling Structure for Gas Turbine Application written by Shan Huang and published by . This book was released on 2016 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Numerical Investigation of Internal Two-Pass Gas Turbine Cooling Channels Under the Influence of Rotation

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ISBN 13 : 9783843945097
Total Pages : pages
Book Rating : 4.9/5 (45 download)

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Book Synopsis Numerical Investigation of Internal Two-Pass Gas Turbine Cooling Channels Under the Influence of Rotation by : Michael Göhring

Download or read book Numerical Investigation of Internal Two-Pass Gas Turbine Cooling Channels Under the Influence of Rotation written by Michael Göhring and published by . This book was released on 2020 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: