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    Computation of turbulent flow over highly curved configuration using a conventional two-equation turbulence model

    , Article 45th AIAA Aerospace Sciences Meeting 2007, Reno, NV, 8 January 2007 through 11 January 2007 ; Volume 9 , 2007 , Pages 6262-6275 ; 1563478900 (ISBN); 9781563478901 (ISBN) Zakyani, M ; Taeibi Rahni, M ; Sharif University of Technology
    American Institute of Aeronautics and Astronautics Inc  2007
    Abstract
    A new procedure for simulating turbulent flow in three-dimensional arbitrary geometries is presented. Finite volume method using physical covariant velocities on a staggered grid arrangement was used in this investigation. This work is an extension of previous successful work to three-dimensional cases. The ability of the new algorithm was tested using a conventional two-equation turbulence model on a highly separated turbulent flow test case. The low Reynolds number k-ω turbulence model of Wilcox was utilized to evaluate its capability in modeling highly curved flows. Turbulent flow over a three-dimensional hill, which is appropriate in assessment of ability of turbulence models in... 

    Investigation of a Turbulent Flow Over a Moving Circular Cylinder, Using Standard Lattice Boltzmann Method

    , M.Sc. Thesis Sharif University of Technology Abdali, Pedram (Author) ; Taeibi Rahni, Mohammad (Supervisor)
    Abstract
    In recent years, LBM has shown to be a suitable computational method for most flow simulations. Its simplicity, adaptability for complex geometries, and capability in parallel processing are among many reasons for broad implementation of LBM these days. In this research, we have tried to take advantage of these features in the simulation of a turbulent flow over a moving circular cylinder at low CPU cost. In order to use LBM in a high Reynolds number incompressible flow over a moving solid body, one needs to pay special attention to grid quality, curved solid wall boundary condition, turbulence model, moving boundary, etc. In order to obtain a suitable practical LBM computer code, the... 

    The effects of baffle plate on soot nano-aerosol and pollutant productions in a JP-fueled combustor

    , Article 54th AIAA Aerospace Sciences Meeting, 2016, 4 January 2016 through 8 January 2016 ; 2016 ; 9781624103933 (ISBN) Darbandi, M ; Ghafourizadeh, M ; Schneider, G. E ; Sharif University of Technology
    American Institute of Aeronautics and Astronautics Inc, AIAA  2016
    Abstract
    In this paper, the effects of a baffle plate on flame deflection and its throttling are investigated numerically in a combustor consuming jet propellant JP. We study the plate effects on the resulting soot volume fraction, soot particles diameter, mass fractions of carbon monoxide (CO), carbon dioxide (CO2), and benzene (C6H6). We use a two-equation turbulence model, a PAH-inception two-equation soot model imposing oxidation due to OH agents, a detailed chemical kinetic consisting of 121 species and 2613 elementary reactions, and the flamelet combustion model to perform the current study. We also take into account the turbulence-chemistry interaction using the presumed-shape probability... 

    Numerical calculation of turbulent reacting flow in a model gas-turbine combustor

    , Article 41st AIAA Thermophysics Conference, 22 June 2009 through 25 June 2009 ; 2009 ; 9781563479755 (ISBN) Darbandi, M ; Ghafourizadeh, M ; Schneider, G. E ; Sharif University of Technology
    Abstract
    In this work, an efficient bi-implicit strategy is suitably developed within the context of a hybrid finite volume element method to solve axisymmetric turbulent reactive flow in a model gas turbine combustor. Based on the essence of a control-volume-based finite-element method, the formulation benefits from the geometrical flexibility of the finite element methods while the discrete algebraic governing equations are derived through applying the conservation laws to discrete cells distributed in the solution domain. To enhance the efficiency of method, we extend the physical influence upwinding scheme to cylindrical coordinates. This extension helps to improve the advection flux... 

    Numerical investigation of supercritical combustion of H2-O2

    , Article Energy and Fuels ; Volume 32, Issue 3 , 2018 , Pages 3851-3868 ; 08870624 (ISSN) Mardani, A ; Barani, E ; Sharif University of Technology
    American Chemical Society  2018
    Abstract
    This study investigates GH2/LOX coaxial jet flame at trans- and supercritical conditions using the Reynolds averaged Navier-Stokes approach. Four two-equation-turbulence models, three real equation of states, two chemical mechanisms, and three different chamber pressures are examined. Predictions show good agreement with measurements qualitatively and quantitatively. Based on the results, the predictions of the Soave-Redlich-Kwong equation of state (EOS) are closer to the experiment, while the Aungier-Redlich-Kwong EOS has more deviation than the others. Moreover, the k-ω shear stress transport model has better performance than the other turbulence models. It is also found that the flow... 

    Evaluation of rans approach in predicting the physics of incompressible turbulent jets-into-crossflow

    , Article ASME International Mechanical Engineering Congress and Exposition, IMECE 2007, Seattle, WA, 11 November 2007 through 15 November 2007 ; Volume 8 PART A , 2008 , Pages 683-698 ; 0791843025 (ISBN); 9780791843024 (ISBN) Javadi, K ; Taeibi Rahni, M ; Darbandi, M ; Sharif University of Technology
    2008
    Abstract
    This work is conducted with evaluation of different turbulence models capabilities in predicting three dimensional jet-into-crossflow (JICF) interactions. For this purpose, first of all, comprehensive discussions on the near wall flow complexities due to discharge of a jet into a crossflow are presented. In this regards, large scale coherent structures such as: counter rotating vortex pairs (CRVP's), near wall secondary motions, horseshoe vortices, and wall jets like are discussed. Secondly, the abilities of different turbulence models in predicting such flows (JICF) are evaluated. Our evaluation is based on three points of view including: 1) JICF characteristics, 2) computed location, and... 

    Dual Lagrangian modeling and Lyapunov-based control of four-wire three-level three-phase NPC voltage-source rectifier

    , Article 2012 11th International Conference on Environment and Electrical Engineering, EEEIC 2012, Venice, 18 May 2012 through 25 May 2012 ; 2012 , Pages 744-751 ; 9781457718281 (ISBN) Mehrasa, M ; Abedi, A ; Ahmadigorji, M ; Reykandeh, M. A ; Sharif University of Technology
    IEEE  2012
    Abstract
    An ac neutral wire is connected to the midpoint of the dc bus of the three level/phase NPC rectifiers and then a new dual Lagrangian model of the rectifier is presented in this paper. At first, the load current can be obtained in two forms: 1. the load current involving the current of capacitor C1 2. The load current involving the current of capacitor C2 and then the new model is founded based on the superposition law, the load current and The Euler-Lagrange description of the rectifier. The new model is two nonlinear state space equations and as a result we define two positive definite Lyapunov function candidates based on two equations. Finally two Lyapunov-based controllers are designed...