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    A preconditioned euler flow solver for simulation of helicopter rotor flow in hover

    , Article Computational Fluid Dynamics 2010 - Proceedings of the 6th International Conference on Computational Fluid Dynamics, ICCFD 2010 ; 2011 , Pages 479-484 ; 9783642178832 (ISBN) Hejranfar, K ; Moghadam, R. K ; National Aeronautics and Space Administration; European Office for Aerospace Research and Development ; Sharif University of Technology
    Abstract
    In the present study, a preconditioned Euler flow solver is developed to accurately and efficiently compute the inviscid flowfield around hovering helicopter rotor. The preconditioning method proposed by Eriksson is applied. The three-dimensional preconditioned Euler equations written in a rotating coordinate frame are solved by using a cell-centered finite volume Roe's method on unstructured meshes. High-order accuracy is achieved via the reconstruction of flow variables using the MUSCL interpolation technique. Calculations are carried out for an isolated rotor in hover for different conditions and the computed surface pressure distributions are compared with the experimental data. The... 

    A high-order accurate unstructured spectral difference lattice Boltzmann method for computing inviscid and viscous compressible flows

    , Article Aerospace Science and Technology ; Volume 98 , 2020 Hejranfar, K ; Ghaffarian, A ; Sharif University of Technology
    Elsevier Masson SAS  2020
    Abstract
    In the present work, the spectral difference lattice Boltzmann method (SDLBM) is implemented on unstructured meshes for the solution methodology to be capable of accurately simulating the compressible flows over complex geometries. Both the inviscid and viscous compressible flows are computed by applying the unstructured SDLBM. The compressible form of the discrete Boltzmann–BGK equation with the Watari model is considered and the solution of the resulting system of equations is obtained by applying the spectral difference method on arbitrary quadrilateral meshes. The accuracy and robustness of the unstructured SDLBM for simulating the compressible flows are demonstrated by simulating four... 

    Assessment of three preconditioning schemes for solution of the two-dimensional Euler equations at low Mach number flows

    , Article International Journal for Numerical Methods in Engineering ; Volume 89, Issue 1 , 2012 , Pages 20-52 ; 00295981 (ISSN) Hejranfar, K ; Kamali Moghadam, R ; Sharif University of Technology
    Abstract
    Three preconditioners proposed by Eriksson, Choi and Merkel, and Turkel are implemented in a 2D upwind Euler flow solver on unstructured meshes. The mathematical formulations of these preconditioning schemes for different sets of primitive variables are drawn, and their eigenvalues and eigenvectors are compared with each other. For this purpose, these preconditioning schemes are expressed in a unified formulation. A cell-centered finite volume Roe's method is used for the discretization of the preconditioned Euler equations. The accuracy and performance of these preconditioning schemes are examined by computing steady low Mach number flows over a NACA0012 airfoil and a two-element... 

    A comparative study of two preconditioners for solving 3D inviscid low speed flows

    , Article Applied Mechanics and Materials ; Volume 110-116 , 2012 , Pages 423-430 ; 16609336 (ISSN) ; 9783037852620 (ISBN) Hejranfar, K ; Moghadam, R. K ; Sharif University of Technology
    2012
    Abstract
    In the present study, two preconditioners proposed by Eriksson, and Choi and Merkel are implemented on a 3D upwind Euler flow solver on unstructured meshes. The mathematical formulations of these preconditioning schemes for the set of primitive variables Q→p 1=[ρ u v , w p] T are drawn and their eigenvalues and eigenvectors are compared with each others. A cell-centered finite volume Roe's method is used for discretization of the 3D preconditioned Euler equations. The accuracy and performance of these preconditioning schemes are examined by computing low Mach number flows over the ONERA M6 wing for different conditions  

    Study of subsonic-supersonic gas flow through micro/nanoscale nozzles using unstructured DSMC solver

    , Article Microfluidics and Nanofluidics ; Volume 10, Issue 2 , February , 2011 , Pages 321-335 ; 16134982 (ISSN) Darbandi, M ; Roohi, E ; Sharif University of Technology
    2011
    Abstract
    We use an extended direct simulation Monte Carlo (DSMC) method, applicable to unstructured meshes, to numerically simulate a wide range of rarefaction regimes from subsonic to supersonic flows through micro/nanoscale converging-diverging nozzles. Our unstructured DSMC method considers a uniform distribution of particles, employs proper subcell geometry, and follows an appropriate particle tracking algorithm. Using the unstructured DSMC, we study the effects of back pressure, gas/surface interactions (diffuse/specular reflections), and Knudsen number on the flow field in micro/nanoscale nozzles. If we apply the back pressure at the nozzle outlet, a boundary layer separation occurs before the... 

    Evaluation of seepage problem under a concrete dam with finite volume method

    , Article Proceedings of the 7th IASME / WSEAS International Conference on Fluid Mechanics and Aerodynamics, FMA '09, 20 August 2009 through 22 August 2009 ; 2009 , Pages 34-40 ; 9789604741069 (ISBN) Shamsai, A ; Abdi Dezfuli, E ; Zebardast, A ; Sharif University of Technology
    Abstract
    In most of countries, underground waters are the most important sources to provide drinking water. So it is necessary to make scheme and to do high protection of to achieve maximum beneficiary. Necessity of this management is going to be felt by developing these sources and human's interference. However, in the past overtopping phenomenon was the first reason of dam's destruction, but nowadays by increasing of spate design's period, the significant problem that researchers are interfere with, is seepage problem. The purpose of solving the underground problems is to procure height of water as a function of coordinate and time. In observation of practical industries, we can use the...