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    Numerical Simulation of A Vortex Cooled Combustion Chamber

    , M.Sc. Thesis Sharif University of Technology Azardar, Milad (Author) ; Farshchi, Mohammad (Supervisor)
    Abstract
    The aim of the present research is to investigate the combustion chamber cooling with vortex method in presence of kerosene and liquid oxygen as propellants. For this purpose, a part of oxidizer is entered into the cylindrical combustion chamber tangentially (from bottem of the chamber), and creates a vortex flow (outer vortex). With motion of created outer vortex along the wall and eventually hit its top wall (the head of the chamber), secondary vortex (inner vortex) occurs along the center line, with a downward direction (opposite to the primary vortex). The fuel and other part of the oxidizer injection is also carried in the head of chamber, so by mixing the fuel and oxidizer that happens... 

    Design and Analysis of Hot Gas Diffuser for High Altitude Simulation

    , M.Sc. Thesis Sharif University of Technology Mirbabaei, Ahmad Reza (Author) ; Farahani, Mohammad (Supervisor) ; Fooladi, Nematollah (Co-Advisor)
    Abstract
    In order to test the performance of engines used at high altitudes, a vacuum simulator system is used. In the vacuum test stand the supersonic exhaust diffuser is used to create the vacuum conditions and the automatic discharge of combustion gases into the atmosphere. usually, the exhaust gas temperature of the engine nozzle is much higher than the temperature that steel body of diffuser can stand (above 2500 K). The purpose of this study is to design and analyze a cooling system to protect the diffusers body. In this study, first by comparing different cooling methods, a spray-cooled water treatment method has been selected for the problem. A new algorithm for designing a spray cooling... 

    Experimental Investigation on Interaction of Three Converging Jets

    , M.Sc. Thesis Sharif University of Technology Kazemi, Sajad (Author) ; Kebriaee, Azadeh (Supervisor)
    Abstract
    In this thesis the instability regimes of the liquid sheet resulted from interactions of three converging jets is investigated. To this end, the shadowgraphy method is used. All the experiments have been done under the atmospheric pressure by using water as the jet fluid. The injectors are orifice ones.In our study, the effects of changing the jet velocities and changing the three jets’ structure (planar and non-planar) in having different liquid sheet shapes are investigated.Although so many researches have been done on interactions of two converging jets until now, there is almost not any researches about interactions of three converging jets. Considering this, this thesis topic is novel,... 

    Develoment of Droplet Velocimetry Method Using Shadowgrapy

    , M.Sc. Thesis Sharif University of Technology Abbasi Zarrin, Fatemeh (Author) ; Kebriaee, Azadeh (Supervisor)
    Abstract
    Injection of liquid fuel in the cross-flowing air provides a means of higher penetration, rapid mixing of liquid fuel and air, and is encountered in many engineering applications. Air-breathing propulsion systems (e.g. gas turbine combustors, ramjets, and scramjets), liquid rocket engines,cooling sprays for turbine blades, and injection of fuel in the afterburners are examples of such applications. The identification of microscopic characteristics is one of the basic methods of atomizer examination, which has not been taken into account due to inadequate experimental equipment. In the present study, droplet mono-frame velocimetry and size distribution of secondary atomization in a pressure... 

    Experimental Study on Spray Output from Small Scale Swirl Injector

    , M.Sc. Thesis Sharif University of Technology Ghodrati, Hossein Ali (Author) ; Morad, Mohammad Reza (Supervisor) ; Kebriaee, Azadeh (Supervisor) ; Ramezani, Ali Reza (Co-Supervisor)
    Abstract
    An injector is one of the most important components of the two components chemical propulsion system used in satellite control. The design of an injector is a complicated and time-consuming process and is largely dependent on laboratory data. In this study, the spray characteristics obtained from a small scale swirl injector under different operating conditions have been experimentally measured in a laboratory environment, such as the injector discharge coefficient, spray cone angle, and the distribution of droplets in the field. To calculate the discharge coefficient, the flow rate of the injector has been measured for different operating pressures. The shooting method and image processing... 

    A Study on Morphology, Structure and Properties of Silver and Gold Coatings Applied by a Chemical Reduction Deposition Method Using Double-Spray Device

    , M.Sc. Thesis Sharif University of Technology Bakhshizadeh, Ali (Author) ; Dolati, Abolghasem (Supervisor)
    Abstract
    Silver and gold are precious, expensive metals and are used in various applications, such as jewellery and ornamentals, electronics and optics. In the present study, soda-lime glass surfaces firstly were activated with acidic stannous chloride solution. Then, silver and gold were coated on these surfaces via simultaneous spraying of two solution: A silver- or gold-complex bearing solution and a reducing agent (Dextrose for Ag and H2O2 for Au) bearing solution. For silver coating, the effect of various parameters such as time, reducing agent concentration, number of passes, presence and concentration of Urotrpin and Decamethylcyclopentasiloxane (DMCPS) as microstructural modifiers and... 

    Time Accurate 3D Analysis of Liquid Jet Breakup Dynamics Using the Image Analysis Techniques

    , M.Sc. Thesis Sharif University of Technology Khademi, Hengameh (Author) ; Farshchi, Mohammad (Supervisor)
    Abstract
    The liquid breakup analysis and spray characteristics measurement of atomizer are very essential for the numerical modeling of the primary atomization in combustion chambers. The atomization process is irregular and random nature and is a chaotic phenomenon. This study was motivated by the lack of temporal analysis of the breakup process especially for the first and second wind-induced breakup regimes and the atomization regime. The aim of this study was to determine the location, velocity and structures of breakup liquid jet at different outlet pressures from 0.3 bar to 50 bar. The results indicate that the breakup length, ligament size, and the breakup time period are randomly varied in... 

    Experimental Study of Spray Pattern of Two Impinging Jets of Non-Newtonian Gel Fluid Containing Aluminum Nanoparticles

    , M.Sc. Thesis Sharif University of Technology Jafari, Maryam (Author) ; Kebriaee, Azadeh (Supervisor)
    Abstract
    In most of the studies conducted on the physics of the outflow from impinging jet injectors, Newtonian fluids have been used for their research and experiments. These studies have investigated the effect of factors such as geometrical parameters of the injector and physical properties of the fluid on different regimes resulting from the impact of the jet stream; Unfortunately, very few studies have been conducted on how to form spray and atomization in gel non-Newtonian fluids containing nanoparticles to investigate the above factors when using impinging jet injectors. Furthermore, although the addition of nanoparticles has advantages for better combustion, there are still problems in... 

    Experimental Study of Liquid Sheet Breakup in Cross Flow

    , Ph.D. Dissertation Sharif University of Technology Olyaei, Ghader (Author) ; Kebriaee, Azadeh (Supervisor)
    Abstract
    Injecting liquid fuel into the cross flow of air provides high penetration of the liquid, rapid mixing with air, and increased efficiency. This method has widespread applications in the propulsion systems of gas turbines, scramjets, turbine blade cooling, and fuel injection for engine afterburners. One of the design strategies for future aircraft engines is to reduce pollutants using fuel spray into the cross flow instead of direct jet fuel injection and using renewable energy sources. The applications of cross flows include injecting fluid through rotating pressure injectors in exhaust flows, injecting fluid through pressure-rotating injectors in radial injectors, and using slinger... 

    Study of Self-Cleaning Silica Nano Coatings

    , M.Sc. Thesis Sharif University of Technology Hadinejad Sheikh, Farshad (Author) ; Afshar, Abdollah (Supervisor)
    Abstract
    It has always been a challenge to make self-cleaning coatings based on super-hydrophobic properties that can provide the necessary features to be operational in the industry. One of these necessary features is the ability to easily apply the coating on the substrate and reduce the cost by finding the optimal amount of consumables. Therefore, in this research, at first, it was tried to produce silica nanoparticles with a particle size of less than 011 nm using the Stober method, and then the surface of the synthesized nanoparticles was coated with HDTMS (Hexadecyltrimethoxysilane) to make the silica particles, which are hydrophilic in nature, hydrophobic. According to the conducted studies,...