Amir Eshghinejadfard

ORCID: 0000-0003-4391-5430
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About
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Research Areas
  • Lattice Boltzmann Simulation Studies
  • Aerosol Filtration and Electrostatic Precipitation
  • Fluid Dynamics and Turbulent Flows
  • Particle Dynamics in Fluid Flows
  • Heat and Mass Transfer in Porous Media
  • Generative Adversarial Networks and Image Synthesis
  • Aerodynamics and Acoustics in Jet Flows
  • Fluid Dynamics and Vibration Analysis
  • Wind and Air Flow Studies
  • Aerodynamics and Fluid Dynamics Research
  • Granular flow and fluidized beds
  • Combustion and flame dynamics
  • Radiative Heat Transfer Studies
  • Innovative Microfluidic and Catalytic Techniques Innovation
  • Advanced Combustion Engine Technologies
  • Computational Fluid Dynamics and Aerodynamics
  • Rheology and Fluid Dynamics Studies
  • Image and Signal Denoising Methods
  • Microfluidic and Bio-sensing Technologies

Newcastle University
2024

University of Manchester
2022-2023

Arak University
2022

Otto-von-Guericke University Magdeburg
2014-2019

Max Planck Institute for Dynamics of Complex Technical Systems
2014-2017

Max Planck Society
2014-2017

University Hospital Magdeburg
2014

Isfahan University of Technology
2011

Particles are present in many natural and industrial multiphase flows. In most practical cases, particle shape is not spherical, leading to additional difficulties for numerical studies. this paper, DNS of turbulent channel flows with finite-size prolate spheroids performed. The geometry includes a straight wall-bounded at frictional Reynolds number 180 seeded particles. Three different shapes considered, either spheroidal (aspect ratio λ=2 or 4) spherical (λ=1). Solid-phase volume fraction...

10.1063/1.5002528 article EN cc-by AIP Advances 2017-09-01

The present study focuses on the behaviour of fully resolved oblate spheroids in turbulent channel flows using lattice Boltzmann method (LBM). Mean and maximum drag reductions 1.3 % 4.4 %, respectively, are observed at a solid-phase volume fraction 10 by aspect ratio $\unicode[STIX]{x1D706}=1/3$ equivalent diameter $D_{eq}/H=1/6.5$ . spheres found to be different near-wall region, where spheroids, contrast spheres, do not augment turbulence. Strong reduction spanwise wall-normal fluid...

10.1017/jfm.2018.441 article EN Journal of Fluid Mechanics 2018-06-21

In many cases, multi-species and/or thermal flows involve large discrepancies between the different diffusion coefficients involved — momentum, heat and species diffusion. context of classical passive scalar lattice Boltzmann (LB) simulations, scheme is quite sensitive to such discrepancies, as relaxation flow fields are tied together through their common spacing time-step size. This in turn leads at least one coefficient, [Formula: see text] being either very close 0.5 or much larger than...

10.1142/s0129183117501418 article EN International Journal of Modern Physics C 2017-12-01

The resolution of small near-wall eddies encountered in high-Reynolds number flows using large eddy simulation (LES) requires very fine meshes that may be computationally prohibitive. As a result, the use wall-modeled LES as an alternative is becoming more popular. In this paper, domain decomposition (NDD) approach was originally developed for Reynolds-averaged Navier–Stokes simulations (RANSs) extended to hybrid RANS/LES zonal decomposition. algorithm implemented two stages. First, solution...

10.3390/math11204340 article EN cc-by Mathematics 2023-10-19

Many natural and industrial processes involve transport of solid particles. This research reports sedimentation modes a single cold elliptical particle with an aspect ratio 2 in narrow hot channels. Prior on settling non-isothermal particles was limited to wide vertical A constant non-dimensional temperature Tp∗=0 initial orientation θ0=π/3 between its major axis horizontal is released fluid. Fluid Prandtl number 7, Tf,0∗=1. Simulations are based in-house lattice-Boltzmann solver two...

10.1016/j.tsep.2022.101519 article EN cc-by Thermal Science and Engineering Progress 2022-10-26

To mitigate the high computational cost associated with resolving small near-wall eddies in large eddy simulation (LES) while achieving acceptable accuracy, this work extends implicit domain decomposition (INDD) method to a hybrid Reynolds-averaged Navier–Stokes (RANS)/LES zonal approach. In framework, LES solution is first computed using Robin-type (slip) wall boundary condition on coarse mesh. This then iteratively corrected region based an updated derived from simplified one-dimensional...

10.1063/5.0245498 article EN cc-by Physics of Fluids 2024-12-01

The impact of the collision model employed when simulating fully resolved particles interacting in a fluid is investigated present study. We are using for this purpose p seudo-spectral compressib le Direct Numerical Simulation (DNS) code based on Navier-Stokes equation as well Lattice-Boltzmann Method (LBM), developed our group and coupled with direct-forcing Immersed Boundary (IBM) to describe particles. Most corresponding literature assumes that does not have significant flow field....

10.1115/fedsm2014-21447 article EN 2014-08-03

Near-wall turbulence modelling with the use of large eddy simulation (LES) is computationally costly since it requires very fine meshes to resolve small eddies near wall. In this research, we a hybrid zonal RANS/LES decomposition that based on near-wall domain method initially developed for Reynolds averaged Navier-Stokes equations (RANS). The solution achieved in two stages. First, computed entire region using LES coarse grid specially derived slip boundary conditions at then recomputed...

10.1615/ichmt.thmt-23.110 article EN 2023-01-01

Near-wall turbulence modelling with the use of large eddy simulation (LES) is computationally costly since it requires very fine meshes to resolve small eddies near wall. In this research, we a hybrid zonal RANS/LES decomposition that based on near-wall domain method initially developed for Reynolds averaged Navier-Stokes equations (RANS). The solution achieved in two stages. First, computed entire region using LES coarse grid specially derived slip boundary conditions at then recomputed...

10.1615/thmt-23.110 article EN 2023-01-01
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