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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... 

    Investigation of luminous/nonluminous radiation in a vortex engine

    , Article 2007 5th Joint ASME/JSME Fluids Engineering Summer Conference, FEDSM 2007, San Diego, CA, 30 July 2007 through 2 August 2007 ; Volume 1 SYMPOSIA, Issue PART B , August , 2007 , Pages 1979-1985 ; 0791842886 (ISBN); 9780791842881 (ISBN) Saidi, M. H ; Kargar, M ; Ghafourian, A ; Sharif University of Technology
    2007
    Abstract
    Investigation of radiation heat transfer In vortex engine is an important and new phenomenon in combustion for scientists and combustion researchers. In this research some parts of the combustion chamber wall are insulated using Blanket as a high insulating material. The rate of radiative heat transfer to the chamber wall is calculated using temperature difference between inner and outer surface of chamber. In the experiments this parts are protected from direct contact with hot combustion media using quartz window. The luminous radiative transfer per volume of chamber and also volume of flame in a vortex engine are compared with that in a similar axial flow type engine. A detector sensitive... 

    Spin dynamics characterization in magnetic dots

    , Article Physica B: Condensed Matter ; Volume 399, Issue 2 , 2007 , Pages 81-93 ; 09214526 (ISSN) Mozaffari, M. R ; Esfarjani, K ; Sharif University of Technology
    2007
    Abstract
    The spin structure in a magnetic dot is studied as a function of the exchange coupling strength and dot size within the semiclassical approximation on a discrete lattice. As the exchange coupling is decreased or the size is increased, the ground state undergoes a phase change from a homogeneous single-domain ferromagnet (HSDF) to a spin vortex. The line separating these two phases has been calculated numerically for small system sizes. The dipolar interaction has been fully included in our calculations. Magnon frequencies in such a dot have also been calculated in both phases by the linearized equation of motion method. These results have also been reproduced from the Fourier transform of... 

    Effect of vortex flow on heat transfer to combustion chamber wall

    , Article Journal of Engineering for Gas Turbines and Power ; Volume 129, Issue 2 , 2007 , Pages 622-624 ; 07424795 (ISSN) Ghafourian, A ; Saidi, M. H ; Jahangirian, S ; Abarham, M ; Sharif University of Technology
    2007
    Abstract
    A new experimental facility was designed, fabricated, and tested to model and study the effect of bidirectional swirl flow on the rate of heat transfer to combustion chamber walls. Reduction of this heat transfer can result in time and cost of design and fabrication methods of combustion chambers. The experimental study was performed using propane and air with oxygen as fuel and oxidizer respectively. For similar flow rates, in cases where bidirectional flow was present, wall temperature reductions of up to 70% were observed. In cases where only some of the oxidizer was injected from the chamber end to generate the bidirectional swirl flow, the lowest wall temperature existed. This can be... 

    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... 

    Experimental investigation of heat transfer modes in vortex combustion engines

    , Article Collection of Technical Papers - 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 8 July 2007 through 11 July 2007, Cincinnati, OH ; Volume 6 , 2007 , Pages 5663-5671 ; 1563479036 (ISBN); 9781563479038 (ISBN) Kargar, M ; Saidi, M. H ; Ghafourian, A ; Sharif University of Technology
    2007
    Abstract
    In a vortex engine, oxidizer issues tangentially at the end of the chamber, consequently a cool vortex flows toward the head, being mixed with fuel, a secondary vortex of combustible reactants swirls coaxial with the first vortex to the nozzle exit. Therefore radiation heat transfer from flame to the chamber wall causes to increase wall temperature; meanwhile highly convective coolant flow of outer vortex reduces the wall temperature. In this paper the rate of total heat transfer and radiative heat are measured experimentally and convective cooling is calculated as the difference between the above mentioned quantities. The rate of heat transfer to the chamber wall is calculated using... 

    Swirl flow effects on heat release/luminuos radiation in a vortex engine

    , Article 2006 ASME Joint U.S.- European Fluids Engineering Division Summer Meeting, FEDSM2006, Miami, FL, 17 July 2006 through 20 July 2006 ; Volume 1 SYPMOSIA , 2006 , Pages 1031-1036 ; 0791847500 (ISBN); 9780791847503 (ISBN) Saidi, M. H ; Kargar, M ; Ghafourian, A ; Faisal, M ; Sharif University of Technology
    2006
    Abstract
    Radiation heat transfer as an important phenomenon in combustion applications is an interesting subject for scientists and combustion researchers. Heat release and luminous radiative transfer phenomena in an experimental vortex engine are compared with a similar axial flow type engine. A detector sensitive to emission from C2* excited radically is utilized for the measurement of chemiluminescence emission at the centerline of chamber along all axial positions. The filtered photographs of flame are used to compare total C2* emission from flame. Mixtures of Propane and Butane with air enriched by oxygen are used as fuel and oxidizer. The effects of equivalence ratio and oxidizer mass flow rate... 

    Vortex transport in separating flows and role of vortical structures in reynolds stress production and distribution

    , Article 2005 ASME Fluids Engineering Division Summer Conference, Houston, TX, 19 June 2005 through 23 June 2005 ; Volume 1 PART A , 2005 , Pages 429-436 ; 0791841987 (ISBN); 9780791841983 (ISBN) Yazdani, M ; Khakpour, Y ; Sharif University of Technology
    2005
    Abstract
    In this paper we will present some approaches on Reynolds stress production by vortex transport phenomena and nonlinear vorticity generation in momentum equation. First of all we represent a history of recent works to describe how fluid particle motions can be associated with Reynolds stress through either displacement or acceleration terms. In the next section we will describe how vortex stretching causes the Reynolds stress production and what is the dominant effect near and far from the boundary where viscous effects have to be considered. On the other hand, some vortex considered methodologies such as those synthesize boundary layer, as a collection of vortical objects seem to be... 

    Vortex Transport in Separating flows and Role of Vortical Structures in Reynolds Stress Production and Distribution

    , Article 2005 ASME Fluids Engineering Division Summer Meeting, FEDSM2005, Houston, TX, 19 June 2005 through 23 June 2005 ; Volume 2005 , 2005 , Pages 11-18 ; 0791837602 (ISBN); 9780791837603 (ISBN) Yazdani, M ; Khakpour, Y ; Sharif University of Technology
    2005
    Abstract
    In this paper we will present some approaches on Reynolds stress production by vortex transport phenomena and nonlinear voracity generation in momentum equation. First of all we represent a history of recent works to describe how fluid particle motions can be associated with Reynolds stress through either displacement or acceleration terms. In the next section we will describe how vortex stretching causes the Reynolds stress production and what is the dominant effect near and far from the boundary where viscous effects have to be considered. On the other hand, some vortex considered methodologies such as those synthesize boundary layer, as a collection of vortical objects seem to be... 

    Experimental and theoretical investigation of heat transfer in vortex combustion engines

    , Article 2005 ASME International Mechanical Engineering Congress and Exposition, IMECE 2005, Orlando, FL, 5 November 2005 through 11 November 2005 ; Volume 376 HTD, Issue 1 , 2005 , Pages 319-326 ; 02725673 (ISSN); 0791842215 (ISBN); 9780791842218 (ISBN) Farvardin, E ; Saidi, M. H ; Ghafourian, A ; Sharif University of Technology
    2005
    Abstract
    Heat transfer phenomenon in a recently developed vortex engine has been surveyed. Cooler walls, better combustion performance and more stable relative to the other engines, make these engines very interesting. These advantages have been obtained by using a bidirectional swirl flow, containing a cool outer and a hot inner vortex, traveling upstream and downstream respectively. The most eminent benefit of these combustion chambers, having highly reduced wall temperature, is the result of convective heat release from the wall by the outer vortex. A thorough numerically and experimentally investigation has been performed on radiation and convection heat transfer to realize the exact heat... 

    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... 

    Numerical analysis of wake structure and performance of two oscillatory mechanisms of a foil: Pure pitching and undulating

    , Article Proceedings of the Institution of Mechanical Engineers Part M: Journal of Engineering for the Maritime Environment ; Volume 229, Issue 4 , April , 2015 , Pages 376-396 ; 14750902 (ISSN) Abbaspoor, M ; Ebrahimi, M ; Sharif University of Technology
    SAGE Publications Ltd  2015
    Abstract
    There are various propulsion, maneuvering, and stabilization mechanisms in nature, which can provide inspiration for similar mechanisms in man-made vehicles. This study aims to elucidate and compare the propulsive vortical signature and performance of a foil in two important natural mechanisms of pure pitching and undulatory oscillations. Governing equations are solved with a pressure-based finite volume method solver, in an arbitrary Lagrangian-Eulerian framework domain containing a NACA 0012 foil moving with prescribed kinematics. The results show that in a given Reynolds number (Re), the undulating mechanism produces thrust at a higher Strouhal number (St) and with smaller growth slope,... 

    Numerical analysis of coherent structures in bidirectional swirl combustion chamber

    , Article Computational Thermal Sciences ; Volume 8, Issue 3 , 2016 , Pages 265-289 ; 19402503 (ISSN) Aghakashi, V ; Keshavarz, P. M ; Saidi, M. H ; Sharif University of Technology
    Begell House Inc 
    Abstract
    Analysis and identification of vortex structures and their formation, particularly in swirl flows, have received widespread interest among researchers in the field of fluid mechanics. Due to the importance of vortex structures and their applications in combustion chambers, a special type of combustion chamber, which is called a “bidirectional swirl combustor,” has been investigated in this work. The dependence of vortex structures on the combustion chamber geometry and fuel injection location in cold flow, the effect of hot flow on coherent structures, and the difference between vortex structures in hot and cold flows have been studied as well. A common characteristic which is in combustion... 

    Vortex with fourfold defect lines in a simple model of self-propelled particles

    , Article Physical Review E - Statistical, Nonlinear, and Soft Matter Physics ; Volume 93, Issue 3 , 2016 ; 15393755 (ISSN) Seyed Allaei, H ; Ejtehadi, M. R ; Sharif University of Technology
    American Physical Society  2016
    Abstract
    We study the formation of a vortex with fourfold symmetry in a minimal model of self-propelled particles, confined inside a squared box, using computer simulations and also theoretical analysis. In addition to the vortex pattern, we observe five other regimes in the system: a homogeneous gaseous phase, band structures, moving clumps, moving clusters, and vibrating rings. All six regimes emerge from controlling the strength of noise and from the contribution of repulsion and alignment interactions. We study the shape of the vortex and its symmetry in detail. The pattern shows exponential defect lines where incoming and outgoing flows of particles collide. We show that alignment and repulsion...