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    Modeling and qualitative experiments on swirling bubbly flows: Single bubble with rossby number of order 1

    , Article Journal of Fluids Engineering, Transactions of the ASME ; Volume 125, Issue 2 , 2003 , Pages 239-246 ; 00982202 (ISSN) Magaud, F ; Najafi, A. F ; Angilella, J. R ; Souhar, M ; Sharif University of Technology
    2003
    Abstract
    The behavior of an isolated bubble in a single-phase swirling flow is investigated theoretically and experimentally. The Rossby number is such that the liquid flow can be approximated by a solid-body rotation superposed to a uniform axial velocity. The equations of the motion of the bubble are solved analytically and numerically, by assuming that the bubble is small and does not modify the water flow. Two kinds of bubbles have been considered: clean bubbles and bubbles with a contaminated interface. In the latter case the bubble is treated as a solid sphere. In both cases a critical angular velocity ωc for the rotating device is found. When ω<ωc the trajectory of the bubble is a conical... 

    Numerical analysis of the swirl intensity decay rate for internal turbulent swirling flow

    , 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 1987-1995 ; 0791842886 (ISBN); 9780791842881 (ISBN) Najafi, A. F ; Mousavian, S. M ; Saidi, M. H ; Sharif University of Technology
    2007
    Abstract
    In this research the trend of swirl decay and factors influencing the turbulent swirl flows have been investigated in a fixed pipe. In this regard, turbulent swirling decay flow with solid body rotation has been numerically surveyed using different flow conditions at the pipe inlet. The numerical results have been validated and compared with the existing mathematical relations having satisfactory agreement. Results show that the swirl intensity decay rate has strong dependency on the Reynolds number. On this basis, correlations have been proposed which improves predictions of swirl intensity decay rate at upstream regions and those with high swirl intensity. In addition, analyses have been... 

    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... 

    Numerical Investigation of Two-Phase Flow Contains Water and Oil in Hydrocyclones

    , M.Sc. Thesis Sharif University of Technology Asadi, Mohammad (Author) ; Farhanieh, Bijan (Supervisor)
    Abstract
    Having an efficient and reliable system for oil-water separation is of crucial importance in oil and gas industry. Hydrocyclones have been used for more than a century to separate oil from water as well as sand from liquid or gas. The main objectives of this research are as follows: Determination the hydrocyclone principle of operation, based on computational fluid dynamic simulations. Hydrocyclones, in a spite of simple structure, are widely used in industry such as Petrochemical, Mining, Chemical Industries, Pharmacy, Food and Pulp Industries. The CALC BFC is one phase flow numerical code based on finite volume method and SIMPLEC algorithm. It was extended for simulating the two phase flow... 

    Neural network prediction of a liquid-liquid coaxial swirl injector performance map

    , Article 43rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, 10 January 2005 through 13 January 2005 ; 2005 , Pages 11401-11408 Ghorbanian, K ; Soltani, M. R ; Morad, M. R ; Ashjaee, M ; Sharif University of Technology
    American Institute of Aeronautics and Astronautics Inc  2005
    Abstract
    A general regression neural network technique is applied for design optimization of liquid-liquid coaxial swirl injectors. Phase Doppler Anemometry measurements for velocity and SMD distributions for various Reynolds numbers are used to train the neural network to generate the injector's performance map. Excellent agreement between the predicted values and the measurements is obtained. It is observed that by reducing the number of randomly selected training samples to about one third of the number of prediction points, one may reconstruct the velocity field in the extrapolation regime with an accuracy of 93%. Copyright © 2005 by the American Institute of Aeronautics and Astronautics, Inc.... 

    Numerical Modeling of Bidirectional Swirling Flow in Vortex Engine

    , M.Sc. Thesis Sharif University of Technology Keshavarz Mohammadain, Poorya (Author) ; Saidi, Mohammad Hassan (Supervisor)
    Abstract
    Detecting of coherent structures in bidirectional vortex combustion chamber is the original aim of this project. For this aim a numerical simulation is performed by using OpenFOAM, open-source CFD software. Also influence of fuel nozzle places in formation of coherent structures is analyzed. Effects of combustion in these structures and differences in cold and hot flows are analyzed too. There are papers that present influence of coherent structures in vortex burners and other applications, but based on reviews that are performed in this work, it seems that influence of coherent structures have not seen in bidirectional vortex chambers. So it can be one of innovations of this work. Swirl... 

    Numerical and Experimental Investigation of Gas-Liquid Two-Phases Flow Around Objects with Different Cross Sections

    , M.Sc. Thesis Sharif University of Technology Nouri Gheimassi, Arash (Author) ; Saeedi, Mohammad Hassan (Supervisor)
    Abstract
    Two phase cross flows around a body have seldom been studied until now and considering these flows can play a significant role in long-term reliability and safety of industrial systems. In this paper flow regimes, drag coefficient and void fraction around different cross-section prisms were considered. To achieve this aim, main equations of flow have been developed for investigation of drag coefficient in air-water two phase. Our numerical analyses were performed by a designed and written CFD package which is based on Eulerian-Eulerian approach. Geometries, which have been studied in this article, are: circle, rectangle and triangle, for different aspect ratio and leading edge angle,... 

    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... 

    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... 

    Simulation of turbulent swirling flow in convergent nozzles

    , Article Scientia Iranica ; Volume 19, Issue 2 , 2012 , Pages 258-265 ; 10263098 (ISSN) Nouri-Borujerdi, A ; Kebriaee, A ; Sharif University of Technology
    Abstract
    This work simulates the turbulent boundary layer of an incompressible viscous swirling flow through a conical chamber. To model the pressure gradient normal to the wall, the radial and tangential velocity components across the boundary layer have been calculated by both the integral and numerical methods. The numerical solution is accomplished by finite difference, based on the finite volume method. The results show that the radial and tangential boundary layer thicknesses depend on the velocity ratios, Reynolds number and nozzle angle. The peak of radial and tangential boundary layer thicknesses are located at zL≈0.2 and zL≈0.8 from the nozzle inlet, respectively. Due to the short length of... 

    Analytical and Experimental Investigation of Spray Flame Front in Bidirectional Vortex Flow

    , Ph.D. Dissertation Sharif University of Technology Dehghani, Saeed Reza (Author) ; Saidi, Mohammad Hassan (Supervisor) ; Mozafari, Ali Asghar (Supervisor) ; Ghafourian, Akbar (Supervisor)
    Abstract
    Vortex engine has shown to be a credible substitute in thermal power and aerospace industries mainly due to their advantages such as better mixing, improved combustion, and considerable cooled walls of combustion chamber. The engine geometry and tangential inlet oxidizer create inner and outer vortices rotating in the same angular direction. The inner vortex moves from head to the end of engine in the axial direction and outer vortex moves in the opposite direction. In the vortex engine, vortices affect spray droplets and force them to have a spiral path and apply a centrifugal force on the droplets to push them towards sidewall. Also axial relative velocity of droplets and flow filed act as... 

    Experimental and Numerical Investigation of Bidirectional Swirl Flow Field in Vortex Engine

    , Ph.D. Dissertation Sharif University of Technology Aghakashi, Vahid (Author) ; Saidi, Mohammad Hassan (Supervisor) ; Mozafari, Ali Asghar (Supervisor)
    Abstract
    Investigation of flow field and vortex structures in swirl flows and their velocity components, have received widespread interest among the 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 “bidirectional swirl combustor” has been investigated in this work. Accurate identification of vortex phenomenon and flow structure in vortex engine leads to better design and control of the engine in the field of stability, geometry, cooling and combustion efficiency. Eperimnetal methods in this area are difficult but very valuable and efficient. Numerical methods are... 

    Analytical Solution of the Swirl Flow in Combustion Chamber of a Hybrid Rocket Engine

    , M.Sc. Thesis Sharif University of Technology Mohammad Beiki, Shahab (Author) ; Farahani, Mohammad (Supervisor) ; Rezayi, Hadi ($item.subfieldsMap.e)
    Abstract
    Hybrid engines are one of a variety of chemical propulsion systems that have been given special attention in recent years by various industries such as space and defense. The most important reasons for considering this type of system are its high safety, its affordable price compared with liquid fuel propulsion systems, the possibility of switching on and off and changing thrust. This system has a lot of disadvantages as well. This system cannot meet all the needs of different industries due to the low regression rate and, consequently, the limitation of the operating range, thrusts and special impulse. As a result, increasing the fuel regression rate in these engines can greatly expand... 

    A new approach to the analytical and numerical solution of the bidirectional vortex flow

    , Article 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Cincinnati, OH, 8 July 2007 through 11 July 2007 ; Volume 5 , 2007 , Pages 4856-4869 ; 1563479036 (ISBN); 9781563479038 (ISBN) Jamaly, S. M ; Saidi, M. H ; Ghafourian, A ; Mozafari, A. A ; Dehghani, S. R ; Sharif University of Technology
    2007
    Abstract
    The solution for bulk fluid motion of a bidirectional coaxial vortex for application in vortex engine has been derived. The vortex engine is a novel combustion chamber in which swirl motion of reactants are used to maintain the chamber walls cool. The flow field has been considered both analytically and numerically. The model is based on incompressible, steady, axisymmetric, and non-reactive flow conditions. The governing PDEs are reduced to a system of nonlinear ODEs and then, by a coordinate transformation, their singularity has been relaxed. Solution domain has been decomposed into the inner viscous and outer inviscid regions, then, the velocity and pressure fields are obtained... 

    Swirl effects on spinning solid propellant rocket motor performance

    , Article AIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference, Sacramento, CA, 9 July 2006 through 12 July 2006 ; Volume 6 , 2006 , Pages 4586-4590 ; 1563478188 (ISBN); 9781563478185 (ISBN) Tahsini, A. M ; Mazaheri, K ; Sharif University of Technology
    American Institute of Aeronautics and Astronautics Inc  2006
    Abstract
    Spining is used in some of solid rocket motors to increase the flight trajectory precision or for stability requirements. The angular acceleration due to the spin increases the burning rate of solid propellant and changes the motor performance by increasing the operating pressure and decreasing the burning time. On the other hand, due to the rocket and its grain rotation, the gases injected from propellant surface to the flow field have an initial angular velocity. The angular velocity of each particle increases as it approaches to the center due to the conservation of angular momentum and a reduction in its radial location, although it vanishes close to the central axis due to viscous... 

    Analytical investigation of boundary layer growth and swirl intensity decay rate in a pipe

    , Article Archive of Applied Mechanics ; Volume 81, Issue 4 , 2011 , Pages 489-501 ; 09391533 (ISSN) Maddahian, R ; Kebriaee, A ; Farhanieh, B ; Firoozabadi, B ; Sharif University of Technology
    Abstract
    In this research, the developing turbulent swirling flow in the entrance region of a pipe is investigated analytically by using the boundary layer integral method. The governing equations are integrated through the boundary layer and obtained differential equations are solved with forth-order Adams predictor-corrector method. The general tangential velocity is applied at the inlet region to consider both free and forced vortex velocity profiles. The comparison between present model and available experimental data demonstrates the capability of the model in predicting boundary layer parameters (e.g. boundary layer growth, shear rate and swirl intensity decay rate). Analytical results showed... 

    Turbulent decaying swirling flow in a pipe

    , Article Heat Transfer Research ; Volume 49, Issue 16 , 2018 , Pages 1559-1585 ; 10642285 (ISSN) Aghakashi, V ; Saidi, M. H ; Sharif University of Technology
    Begell House Inc  2018
    Abstract
    In this work, a solution is applied to investigate the heat transfer characteristics in a pipe with turbulent decaying swirling flow by using the boundary layer integral scheme. The governing equation is solved using the forth-order Runge-Kutta scheme resulting in thermal boundary-layer thickness and dimensionless heat transfer coefficient, namely, the Nusselt number. Both forced- and free-vortex profiles are considered for the tangential velocity component. A comparison of the results obtained for the Nusselt number with available experimental data shows that this scheme has good capability in predicting the heat transfer parameters of swirling flow especially in the entrance region of a... 

    The experimental investigation concerning the heat transfer enhancement via a four-point star swirl generator in the presence of water–ethylene glycol mixtures

    , Article Journal of Thermal Analysis and Calorimetry ; Volume 144 , February , 2020 , 167–178 Jafari, M ; Farajollahi, A ; Gazori, H ; Sharif University of Technology
    Springer Netherlands  2020
    Abstract
    In the present study, a new swirling flow generator is studied which aims to enhance the convective heat transfer rate in a heat exchanger tube. This device has a four-point star cross section. The study mainly investigates the effect of swirl generator on heat transfer rate and pressure drop along the test tube which is under a constant and uniform heat flux. The working fluid in the experiments is the water–ethylene glycol mixtures with Prandtl numbers ranging from 5 to 150 at different Reynolds numbers from 12,000 to 27,000. The results clarify the potential of the applied swirl generator to make a significant enhancement in the heat transfer rate with a satisfactory rise in the pressure... 

    Proposal of a Modular Structure and a Load Sharing Strategy among Back to Back Converters for Wind Turbines

    , M.Sc. Thesis Sharif University of Technology Amouzegar Ashtiani, Nima (Author) ; Mokhtari, Hossein (Supervisor)
    Abstract
    The utilization of wind power has been increasing in recent years which lead to enhance the the usage of wind power capacity in the range of MegaWatt. However, due to the limitation ofswitching devices capacity, which exists in power electronic converters, improving the capacity of wind power generation is not accessible. Thus, a feasible solution for this problem is paralleling power electronics converters, which increases both the capacity of power generation and the reliability of wind turbine systems. Nevertheless, paralleling converters may cause a circulating-current which brings current discrepancy, current waveform distortion, power losses, increase in THD of currents, and reduction... 

    Investigation of Interactions of Injectors and Walls in Vortex Engines

    , M.Sc. Thesis Sharif University of Technology Hamzeie, Faraz (Author) ; Mozafari, Ali Asghar (Supervisor) ; Saidi, Mohammad Hassan (Co-Advisor) ; Ghafourian, Akbar (Co-Advisor)
    Abstract
    A new experimental setup was fabricated; equipped with an adjustable chamber’s length, with air tangentially flowing through the wall of vortex engine. In a vortex combustion chamber, the tangential inlet fuel or oxidizer creates both inner and outer vortices which are rotating in the same angular direction. Indeed, inner vortex moves from head to the end of engine in the axial direction; however, outer vortex moves in the opposite direction. This setup was fabricated to see the effect of fuel nozzle characteristics on the wall temperature of the chamber. In a vortex engine, vortices affect spray droplets and force them to have a spiral path. Moreover, relative velocity of droplets and flow...