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    Experimental Study of Formation Damage Reduction during Drilling of Horizontal Wells Using Nanoparticles

    , M.Sc. Thesis Sharif University of Technology Shojaei, Nima (Author) ; Ghazanfari, Mohammad Hossein (Supervisor)
    Abstract
    One the basic challenges during drilling of both vertical and horizontal wellbores is due to mud filtrate invasion into the formation. Addition of nanoparticles to composition of drilling fluid has been recognized as a measure of control and reduction of filtrate invasion. Despite notable advances in formulation of nano-enhanced drilling fluids, effects of surface wettability of nanoparticles on their performance have not been studied with any precision. Moreover, return permeability of a grain packed porous media after extreme invasion by mud filtrate has not been experimentally measured in a radial system, yet. The last but not least, Generation and development of mud cake opposite the... 

    Separation of CO_2from N_2-CO_2Gas Mixture by Facilitated Liquid Membrane

    , M.Sc. Thesis Sharif University of Technology Alihosseinpour, Hossein Ali (Author) ; Bastani, Daruoosh (Supervisor)
    Abstract
    In this research, separation of carbon dioxide from a mixture of CO_2-N_2 with the aid of liquid membrane containing immobilized solution of diethanolamine-triethylene, known as facilitated liquid membrane, (DEA-TEG) in porous and hydrophilic poly vinylidene fluoride (PVDF) substrate was experimentally and theoretically carried out. The effects of DEA concentration, CO_2 partial pressure, and thickness of membrane on permeability coefficient, facilitation factor, permeation rate and selectivity of liquid membranewere investigated and importance of mass transfer resistance in gas phase on permeability or liquid membrane performance was also shown. Reversible reaction of complex formation... 

    Experimental Investigation of the Roughness Effects on the Pressure Distribution and Stationary Crossflow Instability over a Swept wing

    , M.Sc. Thesis Sharif University of Technology Damghani, Hamid (Author) ; Soltani, Mohammad Reza (Supervisor)
    Abstract

    Wind tunnel experiments are conducted to evaluate surface pressure distribution over a semi span swept wing with sweep angle of 33 degrees. The wing section has a laminar flow airfoil similar to that of NACA 6-series airfoils. The tests were conducted at speeds ranging from 50 to 70m/s with and without surface roughness. Surface static pressure was measured on the wing upper surface at three different chordwise rows located at the inboard station, (section 1, 2y/b=0.2), middle station, (section 2, 2y/b=0.43), and outboard station, (section 3, 2y/b=0.78). The differences between pressure distributions on the three sections of the wing were studied and the experimental results showed that... 

    Experimental and Theoretical Investigation on Losses and Modeling Axial Flow Turbine

    , M.Sc. Thesis Sharif University of Technology Hashemi, Ahmad (Author) ; Hajilouy-Benisi, Ali (Supervisor)
    Abstract
    Prediction of axial flow turbine’s performance with different operating conditions due to the high costs and lack of reliable empirical data is always under developing. In this type of turbine, fluid flow is three-dimensional, viscous and highly turbulent. Nowadays, although a relatively detailed picture of the flow field can be obtained by the computational and numerical tools, but using of appropriate loss models in one-dimensional modeling for the performance prediction as well as optimization of the turbine in initial design phases, is a common trend.
    In the current study, aerodynamic losses in the axial flow turbine are investigated. Several loss models for the axial flow turbines... 

    Modeling of Bushehr NPP TG Load Reduction to Zero Test with Using RELAP5 Code and Evaluationof BNPP Safety Reports

    , M.Sc. Thesis Sharif University of Technology Vahman, Navid (Author) ; Ghofrani, Mohammad Bagher (Supervisor) ; Talebi, Majid (Co-Advisor)
    Abstract
    Due to inherent dangerous on human and environment safety in the nuclear power plant has significant importance. In order to ensure the safety of the plant and proper functioning ofits various components,before its operational exploitation, a series of commissioning tests should be conducted according to international standards for nuclear power plants. In addition, safety of the plant can be guaranteed bymodeling of transient states and possible scenarios of accident in different situations.In this research,by gathering geometric data and information about the facilities installed in the plant, modeling of Commissioning test of Bushehr Nuclear Power Plant (BNPP) and its associated accident... 

    Experimental Study on Hydrodynamic Behavior of Drilling Fluid by Fluidizing Granular Materials in an Annulus

    , M.Sc. Thesis Sharif University of Technology Esmailpour, Reza (Author) ; Jamshidi, Saeed (Supervisor) ; Molaei Dehkordi, Asghar (Supervisor)
    Abstract
    During the drilling process, cutting concentration in vertical and inclined wells is a common problem and major issue in designing hydraulic parameters. This is becoming more important in near bit area. Cutting transport usually is affected by several parameters such as mud rheology, flow rate, nozzle size, rotation speed, and mud weight.
    In this work it was aimed to design a new set-up to test all the factors on hole cleaning phenomenon especially in near bit area. The set-up consists of a 16 feet long flow loop, 3.28 feet height of the test section, and 3.33 inches inner diameter of the test section. Each parameter which has an impact on hole cleaning could be varied. The cutting... 

    High Frequency Vibration Analysis of Two Connected Plates by a Beam Interface via EFEA Method

    , M.Sc. Thesis Sharif University of Technology Ghobad, Yoosef (Author) ; Haddadpour, Hassan (Supervisor) ; Mohammad Navazi, Hossein (Co-Advisor)
    Abstract
    In this study, high frequency vibration analysis of two connected plates by a beam interface is carried out using Energy Finite Element Analysis (EFEA). In structural vibration analysis at low frequencies, classical methods such as Finite Element Method or Boundary Element Method present accurate results. But, using these methods at high frequencies requires expense of high calculation cost and time. Therefore, using of statistical methods that are based on average estimates of vibrations, at high frequencies is most popular. EFEA is a method that gives average response of structure at a certain point and frequency band. This method is developed on the basis of finite element analysis of... 

    Experimental Study the Effect of Control Surface on High speed Vessels Maneuvering in Calm Water

    , Ph.D. Dissertation Sharif University of Technology Hajizadeh, Sajjad (Author) ; Seif, Mohammad Saeed (Supervisor) ; Mehdigholi, Hamid (Supervisor)
    Abstract
    Design optimization of ships by taking maneuverability in account has great influence on the performance of the vessels. Thus providing a method to predict the behavior of vessel in the design process is very important. Ship maneuverability is remarkable from different aspects of view. Especially in high speed vessels of various applications and missions’ good maneuverability would be a positive rating for it. For example, military vessels in specific situations need to change the speed and direction and this is a crucial capability of them. Also in accordance to the rules of IMO all of the vessels should perform maneuvering trials and fulfil the minimum requirements. Accordingly, this issue... 

    Simulation of Natural Circulation Test of The Bushehr's VVER-1000 Nuclear Power Plant with RELAP5

    , M.Sc. Thesis Sharif University of Technology Vafa Toroghi, Mojtaba (Author) ; Ghofrani, Mohammad Bagher (Supervisor)
    Abstract
    Safety is an important factor in the nuclear power plants due to its inherent human and environmental hazards. Therefore, in order to ensure the safety of the plant and proper functioning of its various components, a series of commissioning tests should be conducted according to international nuclear power plants standards, before its operational exploitation. On the other hand, safety of the plant can be guaranteed by modeling transient states and possible scenarios of accidents in different situations. In this study, a commissioning test of Bushehr Nuclear Power Plant (BNPP) and its associated accident is modelled by gathering geometric data and information about the facilities... 

    Shear Capacity of Ultra-High Performance Concrete Rectangular Beams

    , Ph.D. Dissertation Sharif University of Technology Pourbaba, Masoud (Author) ; Joghataie, Abdolreza (Supervisor)
    Abstract
    The application of ultra-high performance concrete (UHPC) as an alternative to conventional/ normal concrete (NC) has grown rapidly in recent years. However, there is limited knowledge on its shear behavior, which is essential for developing design guidelines for structural applications. A detailed parametric study was conducted on 38 beam specimens, half of which were made of UHPC and the other half made of NC. To ensure applicability of findings, two types of UHPC mixes were used, a proprietary and a generic mix. Eighteen of the beams were prepared and tested in Tabriz, Iran, while the other 20 were made and tested in Miami, FL. Test parameters included type of concrete (UHPC and NC),... 

    Assembly Line Balancing with Sequence Dependent Setup Times

    , Ph.D. Dissertation Sharif University of Technology Yolmeh, Abdolmajid (Author) ; Kianfar, Farhad (Supervisor)
    Abstract
    In recent years in assembly line balancing area many researchers have focused on identifying and modeling real world situations in assembly lines in order to obtain more suitable model. As a result many generalized models have been developed in assembly line balancing area. However, designing efficient algorithms to solve these generalized problems has just begun. In this study it is aimed to design efficient algorithms to solve one of these generalized problems. Specificcally two hybrid genetic algorithms (GA) are proposed to solve assembly line balancing problem with sequence dependent setup times. Scheduling of tasks in the stations has been less considered in the literature of assembly... 

    An Experimental and Numerical Study on Jet Electrohydrodynamics

    , Ph.D. Dissertation Sharif University of Technology Rajabi, Alireza (Author) ; Morad, Mohammad Reza (Supervisor)
    Abstract
    Liquid jet behavior in an intense electric field is studied experimentally and numerically.Imaging is used in experiments to charactrize jet behavior. Electrospray of ethanol using a simple needle in a wide range of operating conditions is investigated. Liquid meniscus is captured using a high-speed camera and different electrospray modes are described based on involved forces. A new nozzle is invented that broadens the stability margins of the useful cone-jet mode. The physical mechanisms of the new cone-jet is discussed and it is characterized using appropriate dimensionless parameters. A simple jet in presence of a gaseous crossflow and a normal electric field is also studied. The liquid... 

    Identification of Dynamic Charactristics of an Oil Lubricated Bearing by Modal Testing

    , M.Sc. Thesis Sharif University of Technology Rafiee Gazani, Saeed (Author) ; Mohammad Navazi, Hossein (Supervisor)
    Abstract
    In the present work, the dynamic charactristics of an oil lubricated journal bearing are identified by experimental modal test. First other similar articles were studied. Then according to requrements and specifications of the bearing, a test bed is designed and constracted by existing technologies to perform tests and to collect required data. The test bed consists of several parts, including rotary shaft, stator, oil supply pack, dynamic force shaker and various sensors, which are constructed and assembled with very precise tolerances. In order to identify the dynamic coefficients of the bearing, the test process was performed using dynamic and static forces and collecting required data.... 

    Reducing Ships Fuel Consumption by Adjusting Operational Trim and Draft

    , M.Sc. Thesis Sharif University of Technology Kazemipour Esferjani, Alireza (Author) ; Seif, Mohammad Saeed (Supervisor)
    Abstract
    Nowadays, the attempts to reduce fuel consumption, greenhouse gas emissions and atmospheric pollutants, and economic savings, besides alignment with new rules, have been become the top priorities in the marines industry. In order to satisfy these goals, many efforts have been undertaken, including the vessel's trim and draft optimization which has done both experimentally and numerically and also thrust system simulation, to set a logical link between the effects of trim and draft of the ship and the calculated value of the required thrust from simulation to be able to optimize the fuel consumption. In this method, the ship is considered at the specific draft and the trim in bow and stern... 

    Engine Exhaust Temperature Control By Throttling

    , M.Sc. Thesis Sharif University of Technology Sharifi Alhashem, Alireza (Author) ; Hosseini, Vahid (Supervisor)
    Abstract
    Diesel particulate filters (DPFs) are used in active and passive regeneration exhaust systems in order to reduce the soot emission of diesel engines. Soot regeneration process initiates at a certain minimum temperature. In Compression Ignition (CI) engines, the intake is not throttled usually, and load control is carried out by adjusting the amount of fuel injected into the cylinders. Consequently in low load working condition, as the fuel mass decreases, the air to fuel ratio increases that results in lowered exhaust gas temperature. On the other hand, passive regeneration strategies alone are not enough and it should be backed up by an active regeneration system in order to guarantee... 

    Experimental and Numerical Investigation on the Single Drop Liquid-liquid Mass Transfer in the Presence of Magnetic Nano-particles (Ferrofluids) and Magnetic Field

    , Ph.D. Dissertation Sharif University of Technology Memari, Mohammad (Author) ; Molaie Dehkordi, Asghar (Supervisor) ; Seif Kordi, Ali Akbar (Co-Supervisor)
    Abstract
    The main objective of the present work was to improve the turbulence in single drops using ferrofluids (magnetic nanoparticles) in the presence of uniform and oscillating magnetic fields. In this regard, magnetite nanoparticles ($\mathrm{Fe_3O_4}$) were synthesized by co-precipitation method, characterized using DLS, FT-IR, XRD, VSM, and TEM, and their stability was checked by UV-Vis. The obtained results indicate the proper synthesis of nanoparticles with a mean diameter of about 20 nm and by coating their surfaces by silane that were well stabilized in the base fluid. In the numerical section, the governing equations of transport phenomena for a single drop containing magnetic fluids were... 

    Experimental Aerodynamic Modeling of a Rigid Flapping Wing

    , M.Sc. Thesis Sharif University of Technology Bighshdel, Ariyan (Author) ; Pourtakdoust, Hossein (Supervisor)
    Abstract
    Flapping Aerial Vehicles (FAVs) are those kinds of aerial vehicles in which the wings are responsible for simultaneous producing of lift and thrust forces. To provide necessary aerodynamic loads, flapping wings employ various unsteady mechanisms. They often fly at relatively high Angle of Attacks (AoA), respective to the relative flow. The aerodynamic modelling of flapping wing has always been a challenging task. The unspecified assumptions in the existing models, make them almost insufficient in flight simulation applications. Therefore, this paper aims to develop a generalized aerodynamic model. To this aim, a comprehensive investigation has been conducted on some of previous aerodynamic... 

    Aerodynamic Control of Flow Around a Rigid Wing in Flapping Motion Using Geometry Modification Methods

    , M.Sc. Thesis Sharif University of Technology Mohammadi, Mohammad Hossein (Author) ; Ebrahimi, Abbas (Supervisor) ; Farahani, Mohammad (Supervisor)
    Abstract
    The physics of the flow around the wing in the oscillatory motion of the wing has various patterns, including the leading edge vortex, the tip vortex and trailing edge vortex escape. The interaction of these vortices forms a complex flow structure around the wing, which will have a direct effect on the aerodynamic performance of the wing. Therefore, controlling these structures can be considered as a way to improve the performance of the flapping wing. One of the passive flow control techniques that has recently been taken into consideration is a leading-edge protuberance method. Another type of passive flow control is geometric correction, using corrugation method. According to studies, two... 

    Apatite Digestion and Two-step Leaching in Concentrate Sulfuric Acid for Recovery of REEs’ Cerium, Lanthanum, Neodymium and Yttrium

    , M.Sc. Thesis Sharif University of Technology Kolahdooz, Mohammad Reza (Author) ; Yoozbashizadeh, Hossein (Supervisor)
    Abstract
    Nowadays, apatite mineral is one of the most sought for the recovery of rare earth elements. This mineral is also the main source of phosphoric acid production. To achieve this end, apatite has to react with sulfuric acid to give phosphoric acid. This process is called the wet process. During the wet process, more rare elements enter the remaining solids called phosphogypsum (PG). For the dissolution of rare elements, PG, which is the same as chalk, can be leach with an acidic solution. In this project, the phosphate concentrate from Chadormalu iron ore waste after characteristics diagnosis is digested in concentrated sulfuric acid at temperatures below 100 ° C, and then hydration is... 

    Experimental Study of the Effect of Wing Flapping on the Aerodynamic Performance of Tail and the Stability of a Flapping Wing Air Vehicle

    , M.Sc. Thesis Sharif University of Technology Mesmarian, Mohammad Navid (Author) ; Pourtakdoust, Hossein (Supervisor) ; Kiani, Maryam (Co-Supervisor)
    Abstract
    In adaptation with nature, Flapping Wing Arial Robots (FWARs) are flying vehicles that use wing flapping motion to produce lift and thrust forces simultaneously. Wing oscillating motion of FWARs in turn creates an unsteady and turbulent flow field around them that makes their aerodynamic modeling and analysis a complex and formidable task. As a result, experimental aerodynamic investigation of FWARs has been the focus of many researchers in the last few years. Inspired by nature, Bird-like FWARs utilize a tail as an augmented aerodynamic surface during their flight motion. In turn the tail aerodynamics that in general plays an important role in flight stability and control is adversely...