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The effects of hydrodynamics characteristics on mass transfer during droplet formation using computational approach
, Article 2006 ASME International Mechanical Engineering Congress and Exposition, IMECE2006, Chicago, IL, 5 November 2006 through 10 November 2006 ; 2006 ; 08888116 (ISSN); 0791837904 (ISBN); 9780791837900 (ISBN) ; Taeibi Rahni, M ; Bastani, D ; Javadi, K ; Sharif University of Technology
American Society of Mechanical Engineers (ASME)
2006
Abstract
For the reason that flow expansion model (developed in our previous work) for evaluating mass transfer during droplet formation involves with manifest hydrodynamic aspects, in this research computational simulation of this phenomenon was done for characterization of hydrodynamics effects on the mass transfer during droplet formation. For this purpose, an Eulerian volume tracking computational code based on volume of fluid (VOF) method was developed to solve the transient Navier-Stokes equations for the axisymmetric free-boundary problem of a Newtonian liquid that is dripping vertically and breaking as drops into another immiscible Newtonian fluid. The effects of hydrodynamics effects on the...
Estimation of temperature and residence time of carbon black oil furnace industrial reactors
, Article 2006 ASME International Mechanical Engineering Congress and Exposition, IMECE2006, Chicago, IL, 5 November 2006 through 10 November 2006 ; 2006 ; 0791837904 (ISBN); 9780791837900 (ISBN) ; Soltanieh, M ; Sahebdelfar, S ; Bastani, D ; Javadi, K ; Sharif University of Technology
American Society of Mechanical Engineers (ASME)
2006
Abstract
In the absence of powerful rigorous models, in this research a simple but practical method for calculating the temperature and residence time and carbon black yield in oil-furnace reactors is proposed. For this purpose an empirical formula of the form CXHY is assumed for the carbon black feedstock based on typical feedstock used in this industry. Based on the prevailing reactor conditions, thermodynamic considerations and available outlet tail gas from the reactor, a few representative reactions are considered to describe the entire reaction network. These include complete combustion for the fuel and, incomplete combustion and pyrolysis for the feedstock. Carbon black yield can be estimated...
Microgravity modulation effects on free convection problems LBM simulation
, Article Physics of Fluids ; Volume 30, Issue 1 , 2018 ; 10706631 (ISSN) ; Kazemi, K ; Sharif University of Technology
2018
Abstract
In this paper, microgravity modulation effects on free convection in a cavity are investigated using the lattice Boltzmann method. In order to create microgravity modulation, a sinusoidal time-dependent function is considered. Parameters of the flow are chosen such that the maximum Rayleigh number approaches 106. The natural frequency of the system is obtained at first. Afterwards, effects of different frequencies on the flow and heat transfer fields are investigated in detail. Results are presented in four different frequency ratios categorized as (1) ω∗=1200, 1100, 120, and 110; (2) ω∗=18, 15, 13, and 12; (3) ω∗ = 0.75, 0.85, and 0.95; and (4) the last one is considered for natural...
Marangoni instabilities for convective mobile interfaces during drop exchange: Experimental study and CFD simulation
, Article Colloids and Surfaces A: Physicochemical and Engineering Aspects ; Vol. 441, issue , 2014 , pp. 846-854 ; ISSN: 09277757 ; Karbaschi, M ; Bastani, D ; Ferri, J. K ; Kovalchuk, V. I ; Kovalchuk, N. M ; Javadi, K ; Miller, R ; Sharif University of Technology
2014
Abstract
The inflow pattern of liquid into a droplet is studied experimentally using a surface active dye and compared with results of CFD simulations. The results show visual agreement between experiments and simulations. The CFD simulations show also good agreement with the surface tension measured by drop profile analysis tensiometry (PAT). The inflow of the surfactant induces a Marangoni instability caused by the local arrival of the surfactant at the drop surface. The onset of this Marangoni instability observed experimentally has a delay of about 10. s when compared with the simulation results. Different scenarios are discussed, including a boundary layer barrier, a kinetic-controlled...
Numerical study on boundary layer control using CH4[sbnd]H2[sbnd]air Micro-reacting jet
, Article International Journal of Hydrogen Energy ; Volume 41, Issue 47 , 2016 , Pages 22433-22452 ; 03603199 (ISSN) ; Yahyavi Koochaksarai, M ; Javadi, K ; Sharif University of Technology
Elsevier Ltd
2016
Abstract
The focus of present numerical study is on assessment of control of laminar separation bubble phenomenon using Micro-scale combustion actuators in an airfoil with low Reynolds number under surface effect and free flows. In this way, the characteristics of laminar separation bubble such as its formation, geometry, and transition from laminar to turbulent around airfoil SD8020 in attack angles of 5 and 8° are investigated. Following that, the new combustion actuators in Micro-scale, cold, and hot air-jet injection are introduced to control boundary layer flow in terms of eliminating the separation bubble. Some mechanisms are identified for improvement of methane-air premixed flame...
Investigation of the effect of cavitation passive control on the dynamics of unsteady cloud cavitation
, Article Applied Mathematical Modelling ; Volume 64 , 2018 , Pages 333-356 ; 0307904X (ISSN) ; Moctar, O. E ; Javadi, K ; Sharif University of Technology
2018
Abstract
We present an efficient method to control the evolution of unsteady cloud cavitation around the CAV2003 benchmark hydrofoil using passive cavitation controllers so called cavitation-bubble generators (CGs). Cavitation control may be used in many engineering applications, particularly in the marine and turbo machinery field. We first simulated the unsteady cavitating flow around the hydrofoil without CGs using a Partially-averaged Navier–Stokes (PANS) method, and validated the acquired results against experimental data. We coupled the turbulence model with a mass transfer model and successfully implemented it in the open source toolbox OpenFOAM. Next, we studied the effect of different CGs on...
Corrigendum to “Investigation of the effect of cavitation passive control on the dynamics of unsteady cloud cavitation” Journal of Applied Mathematical Modelling 64 (2018) 333–356 (Applied Mathematical Modelling (2018) 64 (333–356), (S0307904X18303305), (10.1016/j.apm.2018.07.015))
, Article Applied Mathematical Modelling ; Volume 72 , 2019 , Pages 716- ; 0307904X (ISSN) ; el Moctar, O ; Javadi, K ; Sharif University of Technology
Elsevier Inc
2019
Abstract
The authors apologize for omitting to acknowledge the prior work of Javadi et al. wherein they used an appendage as a passive controller to stabilize the cavitation on a 2-D hydrofoil [1]. This paper is an extension of the ideas presented in [1]. Herewith, we would like to acknowledge the omission of the mentioned paper through citing this article in the original paper, as listed below. © 2019 Elsevier Inc
Stabilization of cloud cavitation instabilities using Cylindrical Cavitating-bubble Generators (CCGs)
, Article International Journal of Multiphase Flow ; Volume 115 , 2019 , Pages 108-125 ; 03019322 (ISSN) ; el Moctar, O ; Javadi, K ; Sharif University of Technology
Elsevier Ltd
2019
Abstract
Unsteady cloud cavitation phenomenon is an important subject due to its undesirable effects in various applications such as ship propeller, rudder and hydraulic machinery systems. We present an efficient passive control method to control the cavitation instabilities which may be caused by the shedding of cavity structures in the vicinity of the solid surface of an immersible body. We proposed a passive control method so called Cylindrical Cavitating-bubble Generators (CCGs) on the surface of a benchmark hydrofoil and analyzed the effects of this passive controller on the dynamics of the unsteady cloud cavitation. First we modeled the unsteady cavitating flow around the hydrofoil without CCGs...
The investigation of natural super-cavitation flow behind three-dimensional cavitators: Full cavitation model
, Article Applied Mathematical Modelling ; Volume 45 , 2016 , Pages 165-178 ; 0307904X (ISSN) ; Kadivar, Erfan ; Javadi, K ; Javadpour, S. M ; Sharif University of Technology
Elsevier Inc
2016
Abstract
In this study, natural super-cavitating flow around three different conical cavitators with wedge angles of 30°, 45° and 60° is investigated. We apply the k−ϵ turbulence model and the volume of fluid (VOF) technique to numerically study the three-dimensional cavitating flow around the cavitators. The turbulence approach is coupled with a mass transfer model which is implemented into the finite-volume package. Simulations are performed for different cavitation numbers. Finally, the effects of some important parameters such as the cavitation index, inlet velocity, Froude number and wedge angle of cavitators on the geometrical characteristics of the super-cavities are discussed. Our numerical...
The performance of a physical influence scheme in structured triangular grids
, Article 41st Aerospace Sciences Meeting and Exhibit 2003, Reno, NV, 6 January 2003 through 9 January 2003 ; 2003 ; 9781624100994 (ISBN) ; Schneider, G. E ; Javadi, K ; Solhpour, N ; Sharif University of Technology
2003
Abstract
The physical influence scheme has been successfully tested on quadrilateral grids performing noticeable features on collocated finite-volume approaches. This scheme exhibits excellent accuracy even utilizing coarse grid distributions to solve complex flow fields and solution domains. The main objective of this work is to extend the performance of a physical influence scheme to triangular grid applications using a coloacated finite-volume approach. A basic motivation behind this research is to construct more number of control volumes for a fixed number of grid nodes within a specified solution domain. In another words, a simple extension from quadrilateral to triangular grid can double the...
Approach to analytic solution of navier-stokes equation utilizing adomian decomposition method, jet impinging flow application
, Article WSEAS Transactions on Mathematics ; Volume 5, Issue 5 , 2006 , Pages 507-514 ; 11092769 (ISSN) ; Taeibi Rahni, M ; Javadi, K. H ; Hosseinzadeh, S. F ; Sharif University of Technology
2006
Abstract
Adomian decomposition method was employed to obtain an approximate solution to two-dimensional and axisymmetric jet impinging flows in this work. Assumptions have been made to reduce the related full Navier-Stokes equations to a non-linear ordinary differential equation. A trial and error strategy has been used to obtain the constant coefficient in the approximated solution. Velocity Profiles, Shear stresses and displacement thickness were chosen to be compared with accurate numerical data. Sensitivity of the results to the number of terms have been discussed. The results showed for open boundary problems having at least one boundary condition at infinity, the applicable range of the...
On the complexity of isoperimetric problems on trees [electronic resource]
, Article Discrete Applied Mathematics ; Volume 160 Issue 1-2, January, 2012 Pages 116-131 ; Javadi, Ramin ; Sharif Univercity of Technology
Abstract
This paper is aimed at investigating some computational aspects of different isoperimetric problems on weighted trees. In this regard, we consider different connectivity parameters called minimum normalized cuts/isoperimetric numbers defined through taking the minimum of the maximum or the mean of the normalized outgoing flows from a set of subdomains of vertices, where these subdomains constitute a partition/subpartition. We show that the decision problem for the case of taking k-partitions and the maximum (called the max normalized cut problem NCP^M), and the other two decision problems for the mean version (referred to as IPP^m and NCP^m) are NP-complete problems for weighted trees. On...
An approximation technique for jet impingement flow
, Article AIP Conference Proceedings, 22 September 2014 through 28 September 2014 ; Volume 1648 , 2015 ; 0094243X (ISSN) ; 9780735412873 (ISBN) ; Fincher, D ; Taeibi Rahni, T ; Massah, H ; Javadi, K. H ; Sharif University of Technology
American Institute of Physics Inc
2015
Abstract
The analytical approximate solution of a non-linear jet impingement flow model will be demonstrated. We will show that this is an improvement over the series approximation obtained via the Adomian decomposition method, which is itself, a powerful method for analysing non-linear differential equations. The results of these approximations will be compared to the Runge-Kutta approximation in order to demonstrate their validity
Investigation of hydrodynamically dominated membrane rupture, using smoothed particle hydrodynamics–finite element method
, Article Fluids ; Volume 4, Issue 3 , 2019 ; 23115521 (ISSN) ; Taeibi Rahni, M ; Akbarzadeh, A. M ; Javadi, K ; Ahmadi, G ; Sharif University of Technology
MDPI AG
2019
Abstract
The rupturing process of a membrane, located between two fluids at the center of a three-dimensional channel, is numerically investigated. The smoothed particle hydrodynamics (SPH) and the finite element method (FEM) are used, respectively, for modeling the fluid and solid phases. A range of pressure differences and membrane thicknesses are studied and two different rupturing processes are identified. These processes differ in the time scale of the rupture, the location of the rupture initiation, the level of destruction and the driving mechanism. © 2019 by the authors
Numerical prediction on the interaction of a jet and a turbulent boundary layer
, Article 33rd AIAA Fluid Dynamics Conference and Exhibit 2003, Orlando, FL, 23 June 2003 through 26 June 2003 ; 2003 ; 9781624100956 (ISBN) ; Taeibi Rahni, M ; Schneider, G. E ; Javad, K ; Javadi, A ; Sharif University of Technology
2003
Abstract
The interaction of a jet with a turbulent cross-stream is numerically investigated in this work. The interaction creates many different complex vortices which in turn interact with the main and jet flow as well as themselves. Considering a broad range of applications for the jet/turbulent boundary-layer interaction in industries, better design considerations can be achieved if good knowledge of the mixing behaviour is provided. Therefore, a close look on the near and far fields of a jet in a crossflow is provided in this work. The study is fulfilled by developing a semi-implicit pressure-based algorithm incorporated by Reynolds stress model. The results indicate that the flow topology is...
Introducing film cooling uniformity coefficient
, Article Heat Transfer Engineering ; Volume 39, Issue 2 , 2018 , Pages 180-193 ; 01457632 (ISSN) ; Sharif University of Technology
Taylor and Francis Ltd
2018
Abstract
An optimal performance film cooling implies a high cooling effectiveness along with a wide surface cooling coverage. During the past decades, film cooling effectiveness has been well defined with a specific formula to evaluate the quality of a cooling system. However, despite numerous research on film cooling, there is still no explicit parameter to quantify how well a coolant film is spread over a hot surface. This work introduces a new coefficient namely cooling uniformity coefficient (CUC) to evaluate how well a coolant film is spread over a surface that is being cooled. Four different cases at two blowing ratios of 0.5 and 1.5 are studied. Three cases are ordinary single jets with...
Influence of new superhydrophobic micro-structures on delaying ice formation
, Article Colloids and Surfaces A: Physicochemical and Engineering Aspects ; Volume 595 , 2020 ; Taeibi Rahni, M ; Javadi, K ; Davoudian, S. H ; Miller, R ; Sharif University of Technology
Elsevier B.V
2020
Abstract
Drop motion on different types of new proposed micro-structure surfaces has been numerically investigated to find the optimum structure in view point of ice formation delaying. The droplet automatically moves on the inclined surfaces due to gravity forces. To validate the numerical algorithm, three different bench mark problems have been considered. The results indicate that the present algorithm is trustable for the presented numerical simulations. Then the validated numerical approach has been used to simulate droplet motion on nine proposed superhydrophobic surfaces in the same conditions. Comparison the drop motion on different micro-structure surfaces at different time indicate that...
Flow physics exploration of surface tension driven flows
, Article Colloids and Surfaces A: Physicochemical and Engineering Aspects ; Volume 518 , 2017 , Pages 30-45 ; 09277757 (ISSN) ; Moezzi Rafie, H ; Goodarzi Ardakani, V ; Javadi, A ; Miller, R ; Sharif University of Technology
2017
Abstract
Surface tension driven passive micro-pumping relies mainly on the surface tension properties. To have control over surface tension driven passive micro-pumps (STD-PMPs), it is essential to understand the physical background of the fluid flow in these pumps. Hence, the purpose of this work is to give an exploration of the flow physics of a STD-PMP. In this regard, computer simulation is used to give detailed information about the flow pattern and physical phenomena at different conditions. To this end, a droplet of water, with a specified diameter, is placed onto an entry port connected to another droplet at the exit port via a microchannel. The results indicate that the pumping process, in...
Oscillatory transient flow experiments and analysis in circular microchannels
, Article 2006 ASME International Mechanical Engineering Congress and Exposition, IMECE2006, Chicago, IL, 5 November 2006 through 10 November 2006 ; 2006 ; 08888116 (ISSN); 0791837904 (ISBN); 9780791837900 (ISBN) ; Javadi, K ; Krägel, J ; Miller, R ; Kovalchuk, V. I ; Ferri, J. K ; Bastani, D ; Taeibi Rahni, M ; Sharif University of Technology
American Society of Mechanical Engineers (ASME)
2006
Abstract
In this research purely oscillation fluid flow in two microtubes 150 and 250 μM(3.5 mm length) is studied using computational fluid dynamic (CFD) approach and utilizing a new experimental setup developed for dynamic interfacial tension measurement (capillary pressure technique) in the frequency range between 0.2 and 80 Hz. The experiments are done with pure water at a mean temperature of about 25 °C. The results of oscillatory conditions for microtubes of 0.5 mm in diameter have been compared with experimental results for several frequencies. The computational approach was validated by comparison with experimental data of the continuous constant flow through microtubes and also with...
On nodal domains and higher-order Cheeger inequalities of finite reversible Markov processes [electronic resource]
, Article Stochastic Processes and their Applications ; Volume 122, Issue 4, April 2012, Pages 1748–1776 ; Javadi, Ramin ; Miclo, Laurent ; Sharif Univercity of Technology
Abstract
Let LL be a reversible Markovian generator on a finite set View the MathML sourceV. Relations between the spectral decomposition of LL and subpartitions of the state space View the MathML sourceV into a given number of components which are optimal with respect to min–max or max–min Dirichlet connectivity criteria are investigated. Links are made with higher-order Cheeger inequalities and with a generic characterization of subpartitions given by the nodal domains of an eigenfunction. These considerations are applied to generators whose positive rates are supported by the edges of a discrete cycle ZNZN, to obtain a full description of their spectra and of the shapes of their eigenfunctions, as...