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    Experimental Investigation of the Effects of Canard Position on the Flowfield Over the Wing of a Model

    , M.Sc. Thesis Sharif University of Technology Izadkhah, Mohammad (Author) ; Soltani, Mohammad Reza (Supervisor)
    Abstract
    The analysis results of air combat simulations explain fighters succeed at close air combat that are super maneuverable and at high angle of attack controllable. Closed-coupled delta wing/canard configurations play an important role in modern aircraft design. These configurations offer high trimmed lift, improved agility and maneuverability as well, as a potential for increased lift-to drag ratio, all of which make them attractive to study. Experiments were carried out in a subsonic closed circuit wind tunnel over a delta wing model under the influence of canard. Canard was set in two different vertical positions, high and mid, with respect to the wing location. Flowfield measurements were... 

    Experimental Investigation of the Effects of Wing Aspect ratio and its distance from the Tail on the Aerodynamic parameters at high A.O.A

    , M.Sc. Thesis Sharif University of Technology Afshari, Abbas (Author) ; Soltani, Mohammad Reza (Supervisor) ; Hejranfar, Kazem (Supervisor)
    Abstract
    In recent years, requirement to increase projectile performance, leads to a great interest in high angle of attack Aerodynamics. Projectile Maneuverability is a concept which is defined by having the capability to perform at high angles of attack while maintaining attached flow over the tail, rather than a capability of performing a mission in minimum possible duration. Interaction between body, wing and tail vortices can delay vortex breakdown over the wing and as a result may enhance projectile maneuverability. Studies show that wing aspect ratio and tail location have a remarkable influence on the vortices interaction and thus projectile maneuverability. In the present study, a series of... 

    Influence of Tail on the Wing Pressure Distribution of a Model at Different Conditions

    , M.Sc. Thesis Sharif University of Technology Bahman Jahromi, Iman (Author) ; Soltani, Mohammad Reza (Supervisor) ; Ghorbanian, Kaveh (Supervisor)
    Abstract
    Control surfaces are used in combat aircrafts to control the pitching moment and to help the aircraft perform high angle of attack manoeuvres. For delta wing configuration, the flow characteristics around the horizontal tail depend on the wing and tail flow field and their interactions. The flow over delta wing is mainly characterised by strong vortices. These vortices move downstream and affect the tail flow field making the problem more complicated. The goal of this research is to study the effect of tail up wash on the horizontal wing-body- tail configurations in subsonic flow. For this purpose a series of wind tunnel tests were conducted on a model containing a moveable horizontal tail... 

    Mass Transfer Modeling while Formation of Liquid Jet to another Liquid

    , M.Sc. Thesis Sharif University of Technology Safarirad, Mohammad Reza (Author) ; Bastani, Darioush (Supervisor)
    Abstract
    Liquid-liquid extraction is one of most important processes in chemical industries. So determination of operating condition effects is very critical. In this thesis we modeled concentration profile in the jet via mathematical equations and compare with experimental data. The major problem in concentration profile and solving equations is lack of knowledge in velocity profile within the jet was formed. Therefore, different flow models such as piston flow model, parabolic flow model, vortex flow model and a cone flow model was used and terminal concentrations inside the jet compared with laboratory values. Results shows the most accurate model to predict the flow concentration along the... 

    Effect of Delta Wing Leading Edge Vortex on Pressure Distribution of Fuselagein in Subsonic Regime

    , M.Sc. Thesis Sharif University of Technology Sadri, Vahid (Author) ; Soltani, Mohammad Reza (Supervisor) ; Ghorbanian, Kaveh (Supervisor)
    Abstract
    The delta wing has proven to be very useful for the study and understanding of the basic features of separation-induced vortex flows since many aspects of these vortex flows can be generated with this simple shape. A phenomenon of special importance to vortical flows is vortex breakdown. Vortex breakdown remains an important and complicated phenomenon that can have negative or positive effects. The delta wing leading edge vortex is emphases in many experiments. Most of these experiments are focused on the delta wing only.In this research, emphasis is on vortex interaction of delta wing-canard-fuselage configuration. A series of low speed wind tunnel tests were carried out to investigate... 

    Experimental Investigation of Flow Past a Delta Wing Model in Presence of a Canard in Supersonic Regime

    , M.Sc. Thesis Sharif University of Technology Dehghani, Parham (Author) ; Soltani, Mohammad Reza (Supervisor)
    Abstract
    Application of canard next to the wing have been widely used in military industry for decades. Although it’s most application is in supersonic flying objects, It has to do it’s duty in lower air speeds too. The aim of this study was to investigate the influence on the wing due to the presence of canard in supersonic flow regime. But because of the importance of the issue, significant attempts has been conducted in subsonic flow regime. High research volume, Absence of a comprehensive theory in this branch and the local defense industry demand as a developing country on the other hand, delivers the importance and applicability of the subject. Another issue of importance is that the... 

    The Spin-Orbit Interaction and Topological Vortices in Unconventional Superconductors

    , M.Sc. Thesis Sharif University of Technology Hosseinabadi, Hossein (Author) ; Kargarian, Mehdi (Supervisor)
    Abstract
    In this work we introduce a new proposal to realize topological superconductivity. In this model we use a ferromagnetic material with high curie temperature like Nickel in proximity to the surface of a three dimensional topological insulator or equivalently Bismuth which has surface states with strong spin-orbit coupling which makes its surface Hamiltonian similar to the surface of a three dimensional topological insulator.The surface electrons of Bismuth are Dirac fermions with strong spin-orbit interaction. The interaction of surface electrons with magnetic fluctuations in the ferromagnet induces an effective attractive electron-electron interaction among surface electrons upon integration... 

    Effects of Vortical Flows on Hydrodynamics of Boxfish

    , M.Sc. Thesis Sharif University of Technology Oloumi Yazdi, Mohammad Hassan (Author) ; Abbaspour Tehranifard, Madjid (Supervisor) ; Rad, Manoochehr (Supervisor)
    Abstract
    In recent decades, bio-inspired design has become a common approach among engineers. Research and study of biological systems show that these systems are very efficient and consume the least amount of energy in a definite process. Specifically, marine mammals and fishes are great sources of inspiration. As an example, recently vertical axis wind turbine farms have been designed and constructed inspired by schools of fish, to produce more electricity. Boxfishes (Teleostei: Ostraciidae) are known for their hydrodynamic stability and relatively low drag coefficient. Highly maneuverable underwater robots have been designed according to morphology of boxfishes. Furthermore, Mercedes-Benz has... 

    Experimental investigation of Pressure Distribution over Delta Wing in
    Sub/supersonic Speed

    , M.Sc. Thesis Sharif University of Technology Sadeghian, Saeed (Author) ; Soltani, Mohammad Reza (Supervisor)
    Abstract
    Flow characteristics analysis over a wing, is one of the pioneer challenges in super and sub-sonic flow near flying objects. Taking into account of growing rate of low aspect ratio utilization, usually called Delta wings, investigation of vortex behavior over this wings is highly noticeable. In addition, the lack of research in this branch of Aerodynamics inside the country, considering it’s critical application, has doubled the importance of doing research in this filled. Experimental researches on super-sonic flow over a Delta wing is limited and there are not much accurate researches about vortexes in this category of wings. In this work, the main effort is to investigate the phenomena in... 

    3D Numerical Simulation of Two-Phase Immiscible Flow in Axial Vortex Technology and Economic Analysis for Industrial Produced Water Pretreatment Facility in Desalting Plants

    , M.Sc. Thesis Sharif University of Technology Aghaee, Mohammad (Author) ; Roshandel, Ramin (Supervisor) ; Ashjari, Mohammad Ali (Supervisor)
    Abstract
    The phenomenon of vortex flow, is one of the most predominant streams in the nature. This phenomenon yielded by the motion of vortices, produces up to 1000 times acceleration of the Earth’s gravity. The issues of uncontrolled harvesting of oil wells and increase the life of the wells, which cause to increase in the extracted crude salt, reveal the importance of waste management and both handling and refining petroleum. According to global statistics, for every extracted barrel of oil, three barrels of water are yielded. Therefore, 250 million produced water barrels per day is produced.The separator technology with vortex core (brand Voraxial) is one of the latest technologies in waste-water... 

    Design Optimization of Pouring basin in the Shape Casting Process

    , M.Sc. Thesis Sharif University of Technology Zohrevand, Milad (Author) ; Davami, Parviz (Supervisor) ; Tavakoli, Rohollah (Supervisor)
    Abstract
    The pouring basin is a main part in the gating system. The formation of a vortical flow is a big problem occurs during the discharge of melt from the pouring basin. The vortex formation can enter the floating slag and inclusion into the mold. In the case that the vortex is more stronger, a fully air core to the sprue forms and leads to entraining of the air to the mold. These phenomena can decrease the casting quality significantly. Therefore preventing of the vortex is necessary to produce a sound cast. In this study the mechanism of vortex formation is investigated and several solutions are presented to avoid its detrimental effects. For this purpose discharge of a tank is simulated... 

    Design and Performance Analysis of a Reversible Axial Flow Fan and Study of Symmetric Profile Effects

    , M.Sc. Thesis Sharif University of Technology Soltanian, Salman (Author) ; Afshin, Hossein (Supervisor) ; Farhanieh, Bijan (Co-Advisor)
    Abstract
    Smoke must be exhausted, as the first action, in probable fire in subways, underground transportation systems and mines in order to survive people exposed to it. To achieving this purpose, the axial fan should be used to move the smoke to the exit lines. These fans should be had same performances in suction and discharge directions (main and reverse directions). This means flow rate should be the same at main and reverse directions. Therefore, fully reversible axial flow fans should be used in emergency ventilations. The fully reversible axial flow fans have same efficiencies in suction and discharge directions. The symmetric profiles should be used in manufacturing of the blades of these...