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    On the Behavior of Semi-Hinged Double-Angle Connections

    , M.Sc. Thesis Sharif University of Technology Esfahanian, Alireza (Author) ; Mofid, Masood (Supervisor)
    Abstract
    In this thesis, the semi-hinged connections such as double-angle connections, which are welded to the beam web and bolted to the column flange, are investigated. In this study it's tried to establish the effect of clearance setback between beam end and column flange and/or web. When the beam rotates, it is desirable to avoid the bottom flange of the beam bearing against the column as this can induce large forces in the connection. The usual way of achieving this is to ensure that the connection extends at least a few millimeters beyond the end of the beam. For this purpose, several connections are designed and considered, based on two different shear capacities for the beam. For each... 

    Application of a shock-fitted spectral collocation method for computing transient high-speed inviscid flows over a blunt nose

    , Article Journal of Computational Physics ; Vol. 257 , 2014 , pp. 954-980 ; ISSN: 00219991 Najafi, M ; Hejranfar, K ; Esfahanian, V ; Sharif University of Technology
    2014
    Abstract
    Interaction of freestream disturbances with high-speed inviscid flow over a blunt nose is simulated utilizing a shock-fitted spectral collocation method. The unsteady flow computations are made through solving the 2D Euler equations by virtue of such a dissipation-free numerical algorithm for precise unsteady flow simulations. A shock-fitting technique is employed to accurately compute the unsteady shock motions and its interaction with monochromatic freestream disturbances of different conditions. A symmetry condition is proposed to accurately model the both steady and unsteady characters of the symmetry boundary, which allows the use of halved geometries and avoids the extra computational... 

    An improved progressive preconditioning method for steady non-cavitating and sheet-cavitating flows

    , Article International Journal for Numerical Methods in Fluids ; Volume 68, Issue 2 , December , 2012 , Pages 210-232 ; 02712091 (ISSN) Esfahanian, V ; Akbarzadeh, P ; Hejranfar, K ; Sharif University of Technology
    2012
    Abstract
    An improved progressive preconditioning method for analyzing steady inviscid and laminar flows around fully wetted and sheet-cavitating hydrofoils is presented. The preconditioning matrix is adapted automatically from the pressure and/or velocity flow-field by a power-law relation. The cavitating calculations are based on a single fluid approach. In this approach, the liquid/vapour mixture is treated as a homogeneous fluid whose density is controlled by a barotropic state law. This physical model is integrated with a numerical resolution derived from the cell-centered Jameson's finite volume algorithm. The stabilization is achieved via the second-and fourth-order artificial dissipation... 

    Receptivity of hypersonic flow over blunt-noses to freestream disturbances using spectral methods

    , Article Computational Fluid Dynamics 2010 - Proceedings of the 6th International Conference on Computational Fluid Dynamics, ICCFD 2010, 12 July 2010 through 16 July 2010 ; July , 2011 , Pages 357-362 ; 9783642178832 (ISBN) Hejranfar, K ; Najafi, M ; Esfahanian, V ; Sharif University of Technology
    2011
    Abstract
    The receptivity of supersonic/hypersonic flows over blunt noses to freestream disturbances is performed by means of spectral collocation methods. The unsteady flow computations are made through solving the full Navier-Stokes equations in 2D. A shock-fitting technique is used to compute unsteady shock motion and its interaction with freestream disturbances accurately in the receptivity study. The computational results for receptivity of a semi-cylinder at Mach 8 is presented and validated by comparison with available theoretical and numerical results. The study shows significant effects of the viscosity on the receptivity process  

    Practical prediction of supersonic viscous flows over complex configurations using personal computers

    , Article Journal of Spacecraft and Rockets ; Volume 38, Issue 5 , 2001 , Pages 795-798 ; 00224650 (ISSN) Esfahanian, V ; Azimi, A ; Hejranfar, K ; Sharif University of Technology
    2001

    Investigation of flow around a confined elliptical cylinder using the Lattice Boltzmann method

    , Article World Applied Sciences Journal ; Volume 22, Issue 7 , 2013 , Pages 1013-1018 ; 18184952 (ISSN) Taeibi Rahni, M ; Salari, M ; Esfahanian, V ; Sharif University of Technology
    2013
    Abstract
    This paper deals with the investigation of the laminar flow past an elliptical cylinder confined in a channel. In this paper, the Lattice Boltzmann (LB) method is used to simulate flow in two dimensions. The present LB method with the used boundary conditions is validated in simulations of the incompressible flow past a circular cylinder. The simulations are carried out in a range of condition, 0 90 (angle of incidence), 5 Re 100, (Reynolds number) for AR=0.25,0.5 (aspect ratio). The effects of those parameters on the drag and lift coefficients and other flow characteristics of the cylinder are examined in detail. The results demonstrate that the drag and lift coefficients increase with the... 

    A new approach to reduce memory consumption in lattice boltzmann method on GPU

    , Article Journal of Applied Fluid Mechanics ; Volume 10, Issue 1 , 2017 , Pages 55-67 ; 17353572 (ISSN) Sheida, M ; Taeibi Rahni, M ; Esfahanian, V ; Sharif University of Technology
    Isfahan University of Technology  2017
    Abstract
    Several efforts have been performed to improve LBM defects related to its computational performance. In this work, a new algorithm has been introduced to reduce memory consumption. In the past, most LBM developers have not paid enough attention to retain LBM simplicity in their modified version, while it has been one of the main concerns in developing of the present algorithm. Note, there is also a deficiency in our new algorithm. Besides the memory reduction, because of high memory call back from the main memory, some computational efficiency reduction occurs. To overcome this difficulty, an optimization approach has been introduced, which has recovered this efficiency to the original... 

    Dual-code solution procedure for efficient computing equilibrium hypersonic axisymmetric laminar flows

    , Article Aerospace Science and Technology ; Volume 12, Issue 2 , 2008 , Pages 135-149 ; 12709638 (ISSN) Hejranfar, K ; Kamali Moghadam, R ; Esfahanian, V ; Sharif University of Technology
    2008
    Abstract
    An appropriate combination of the thin-layer Navier-Stokes (TLNS) and parabolized Navier-Stokes (PNS) solvers is used to accurately and efficiently compute hypersonic flowfields of equilibrium air around blunt-body configurations. The TLNS equations are solved in the nose region to provide the initial data plane needed for the solution of the PNS equations. Then the PNS equations are employed to efficiently compute the flowfield for the afterbody region by using a space marching procedure. Both the TLNS and PNS equations are numerically solved by using the efficient implicit non-iterative finite-difference algorithm of Beam and Warming. A shock fitting technique is used in both the TLNS and... 

    Implementation of high-order compact finite-difference method to parabolized Navier-Stokes schemes

    , Article International Journal for Numerical Methods in Fluids ; Volume 58, Issue 6 , 2008 , Pages 659-685 ; 02712091 (ISSN) Esfahanian, V ; Hejranfar, K ; Mahmoodi Darian, H ; Sharif University of Technology
    2008
    Abstract
    The numerical solution to the parabolized Navier-Stokes (PNS) and globally iterated PNS (IPNS) equations for accurate computation of hypersonic axisymmetric flowfields is obtained by using the fourth-order compact finite-difference method. The PNS and IPNS equations in the general curvilinear coordinates are solved by using the implicit finite-difference algorithm of Beam and Warming type with a high-order compact accuracy. A shock-fitting procedure is utilized in both compact PNS and IPNS schemes to obtain accurate solutions in the vicinity of the shock. The main advantage of the present formulation is that the basic flow variables and their first and second derivatives are simultaneously... 

    Implementation of high-order compact schemes to the iterative parabolized Navier-Stokes equations

    , Article 25th Congress of the International Council of the Aeronautical Sciences 2006, Hamburg, 3 September 2006 through 8 September 2006 ; Volume 3 , 2006 , Pages 1628-1643 Esfahanian, V ; Hejranfar, K ; Darian, H. M ; Sharif University of Technology
    Curran Associates Inc  2006
    Abstract
    The numerical solution of the parabolized Navier-Stokes (PNS) and globally iterated PNS (IPNS) equations for accurate computation of hypersonic axisymmetric flowfields is obtained by using the fourth-order compact finite-difference method. The PNS and IPNS equations in the general curvilinear coordinates are solved by using the implicit finite-difference algorithm of Beam and Warming type with a high-order compact accuracy. A shock fitting procedure is utilized in both the compact PNS and IPNS schemes to obtain accurate solutions in the vicinity of the shock. The main advantage of the present formulation is that the basic flow variables and their first and second derivatives are... 

    Reduced-order modeling of unsteady flows without static correction requirement

    , Article Journal of Aircraft ; Volume 42, Issue 4 , 2005 , Pages 882-886 ; 00218669 (ISSN) Behbahani Nejad, M ; Haddadpour, H ; Esfahanian, V ; Sharif University of Technology
    American Institute of Aeronautics and Astronautics Inc  2005
    Abstract
    A new reduced-order modeling approach is presented. This approach is based on fluid eigenmodes and without using the static correction. The vortex lattice method is used to analyze unsteady flows over two-dimensional airfoils and three-dimensional wings. Eigenanalysis and reduced-order modeling are performed using a conventional method with and without the static correction technique. In addition to the conventional method, eigenanalysis and reduced-order modeling are also performed using the new proposed method, that is, without static correction requirement. Numerical examples are presented to demonstrate the accuracy and computational efficiency of the proposed method. Based on the... 

    Assessment of the semi-rigid double-angle steel connections and parametric analyses on their initial stiness using FEM

    , Article Scientia Iranica ; Volume 22, Issue 6 , 2015 , Pages 2033-2045 ; 10263098 (ISSN) Esfahanian, A ; Mohamadi Shooreh, M. R ; Mod, M ; Sharif University of Technology
    2015
    Abstract
    In this paper, the semi-rigid connections, such as Double-angle Web (DW) connections, which are welded to the beam web and bolted to the column ange, are investigated. This study tries to establish the eect of clearance setback between beam end and column ange and/or web. When the beam rotates, it is desirable to avoid bottom ange of the beam bearing against the column as this can induce large forces on the connection. The usual way of achieving this is to ensure that the connection extends at least a few millimeters beyond the end of beam. For this purpose, several connections are designed and considered based on two dierent shear capacities for the beam. For each connection, two dierent... 

    Receptivity of High-Speed Flows over Blunt Noses using Spectral Methods

    , Ph.D. Dissertation Sharif University of Technology Najafi, Mehdi (Author) ; Hejranfar, Kazem (Supervisor) ; Esfahanian, Vahid (Co-Advisor)
    Abstract
    The receptivity, transition and stability mechanisms of supersonic and hypersonic boundary layers to freestream disturbances are one of the most complex studies in fluid mechanics. It is well known that turbulent flows generate much higher shear forces on the surface of vehicles and hence much higher viscous heating rates than a laminar flow would at the same flight conditions. Therefore, the accurate prediction of boundary layer behavior is a critical part of the aerodynamic design of high-speed vehicles and thermal protection systems. Formation of a bow shock in front of the vehicle makes the receptivity of flow-field more complex than and different from those of low-speed subsonics. Since... 

    Simulation and Analysis of a Reactive Flow in a Porous Media, Using LBM and GPU

    , Ph.D. Dissertation Sharif University of Technology Sheida, Mojtaba (Author) ; Taeibi Rahni, Mohammad (Supervisor) ; Esfahanian, Vahid (Co-Advisor)
    Abstract
    In this research, surface reaction phenomenon in porous media has been numerically simulated in pore scale. The main interesting part in this kind of physics is surface reaction exposed to a flow field. In this regard, an in-house code, based on LBM was developed. To speed-up our simulation, parallel computing was used on a GPU platform leading to a significant speed-up. Also, to model a real complex geometry, X-CT and MRI medical imaging technique were used to accurately model several complex 3D geometries. While, image processing technique was used to model our 2D geometries. The basic equilibrium equation of isopropanol dehydrogenation was considered to simulate and to analize chemical... 

    Numerical-Experimental geometric optimization of the ahmed body and analyzing boundary layer profiles

    , Article Journal of Optimization Theory and Applications ; 2021 ; 00223239 (ISSN) Abdolmaleki, M ; Mashhadian, A ; Amiri, S ; Esfahanian, V ; Afshin, H ; Sharif University of Technology
    Springer  2021
    Abstract
    The trade-off between the fuel consumption and drag coefficient makes the investigations of drag reduction of utmost importance. In this paper, the rear-end shape optimization of Ahmed body is performed. Before changing the geometry, to identify the suitable simulation method and validate it, the standard Ahmed body is simulated using k − ω shear stress transport (SST) and k-epsilon turbulence models. The slant angle, rear box angle, and rear box length as variables were optimized simultaneously. Optimizations conducted by genetic algorithm (GA) and particle swarm optimization (PSO) methods indicate a 26.3% decrease in the drag coefficient. To ensure the validity of the results, a... 

    Numerical-Experimental geometric optimization of the Ahmed body and analyzing boundary layer profiles

    , Article Journal of Optimization Theory and Applications ; 2021 ; 00223239 (ISSN) Abdolmaleki, M ; Mashhadian, A ; Amiri, S ; Esfahanian, V ; Afshin, H ; Sharif University of Technology
    Springer  2021
    Abstract
    The trade-off between the fuel consumption and drag coefficient makes the investigations of drag reduction of utmost importance. In this paper, the rear-end shape optimization of Ahmed body is performed. Before changing the geometry, to identify the suitable simulation method and validate it, the standard Ahmed body is simulated using k − ω shear stress transport (SST) and k-epsilon turbulence models. The slant angle, rear box angle, and rear box length as variables were optimized simultaneously. Optimizations conducted by genetic algorithm (GA) and particle swarm optimization (PSO) methods indicate a 26.3% decrease in the drag coefficient. To ensure the validity of the results, a... 

    Numerical-Experimental geometric optimization of the Ahmed body and analyzing boundary layer profiles

    , Article Journal of Optimization Theory and Applications ; Volume 192, Issue 1 , 2022 ; 00223239 (ISSN) Abdolmaleki, M ; Mashhadian, A ; Amiri, S ; Esfahanian, V ; Afshin, H ; Sharif University of Technology
    Springer  2022
    Abstract
    The trade-off between the fuel consumption and drag coefficient makes the investigations of drag reduction of utmost importance. In this paper, the rear-end shape optimization of Ahmed body is performed. Before changing the geometry, to identify the suitable simulation method and validate it, the standard Ahmed body is simulated using k − ω shear stress transport (SST) and k-epsilon turbulence models. The slant angle, rear box angle, and rear box length as variables were optimized simultaneously. Optimizations conducted by genetic algorithm (GA) and particle swarm optimization (PSO) methods indicate a 26.3% decrease in the drag coefficient. To ensure the validity of the results, a... 

    A sequential approach for hybridizing conventional vehicles and an approval example

    , Article 8th Biennial ASME Conference on Engineering Systems Design and Analysis, ESDA2006, Torino, 4 July 2006 through 7 July 2006 ; Volume 2006 , 2006 ; 0791837793 (ISBN); 9780791837795 (ISBN) Esfahanian, M ; Khanipour, A ; Nabi, A ; Fazeli, A. M ; Amiri, M ; Sharif University of Technology
    American Society of Mechanical Engineers  2006
    Abstract
    Hybridization of conventional vehicles is considered an important step to achieve high fuel economy and low emissions. In this study, principle considerations involved in a hybridizing process are discussed and consequently, a sequential approach for designing hybrid components for both series and parallel configurations has been introduced. The so called approach has then been applied to one of the productions of Iran-Khodro Company called SAMAND. Having designed the hybrid components, the conventional SAMAND and its series and parallel hybrid configurations were defined and evaluated using the ADvanced VehIcle SimulatOR (ADVISOR) software. It is observed that compared to the conventional... 

    Rcci Curvature for Metric-Measure Space via Optimal Transport

    , M.Sc. Thesis Sharif University of Technology Taheri, Abolfazl (Author) ; Bahraini, Alireza (Supervisor) ; Ranjbar Motlagh, Alireza (Co-Advisor)
    Abstract
    One of the important questions in mathematics is generalized. In case of metric spaces, one of the questions is: Can we extend notions of Riemannian geometry to arbitrary metric spaces smoothly? Ricci curvature is one of the most important concepts in differential geometry. Ricci curvature is defined for the Riemannian manifold and has many applications in mathematics and physics like Einstein’s equation in relativity theory. There is a good notion for a metric space having “sectional curvature bounded below by K” or “sectional curvature bounded above by K”, due to Alexandrov. Can we define the concept of Ricci curvature in metric space? A motivation for this question comes from Gromov’s... 

    , M.Sc. Thesis Sharif University of Technology (Author) ; Khaloo, Alireza (Supervisor)
    Abstract
    Seismic design codes reduce loads by using response modification factor. Because of the reserved strength in structural elements and capacity of structure to dissipate energy, structures can be designed for lower seismic loads. This factor has modified over time. In this thesis, the effect of the reduction in behavior factor on the response of two kinds of reinforced concrete systems were evaluated. Moment resisting frames and dual systems with different heights and regularity in plan, heve been design according to the behavior factor which is recommended in the 3rd edition of the Iranian codes of practice for seismic resistance design of buildings (Standard No. 2800). Drift and...