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mohammad reza salimi
mohammad reza salimi
Assistant Professor of Aerospace Engineering, Aerospace Research Institute of Iran
在 ari.ac.ir 的电子邮件经过验证
标题
引用次数
引用次数
年份
Heat transfer and entropy generation analysis in a three-dimensional impinging jet porous heat sink under local thermal non-equilibrium condition
MR Salimi, M Taeibi-Rahni, H Rostamzadeh
International Journal of Thermal Sciences 153, 106348, 2020
432020
Compound triple jets film cooling improvements via velocity and density ratios: large eddy simulation
R Farhadi-Azar, M Ramezanizadeh, M Taeibi-Rahni, M Salimi
412011
Computational simulation of temperature and velocity distribution in human upper respiratory airway during inhalation of hot air
V Goodarzi-Ardakani, M Taeibi-Rahni, MR Salimi, G Ahmadi
Respiratory physiology & neurobiology 223, 49-58, 2016
292016
Modified cost analysis integrated with dual parametric sensitivity study for realistic cost assessment of a novel modified geothermal-based multi-generation energy system
A Farajollahi, M Rostami, M Feili, H Ghaebi, MR Salimi
Energy Reports 8, 13463-13483, 2022
232022
Permeability correlation with porosity and Knudsen number for rarefied gas flow in Sierpinski carpets
H Rostamzadeh, MR Salimi, M Taeibi-Rahni
Journal of Natural Gas Science and Engineering 56, 549-567, 2018
202018
Heat transfer analysis of a porously covered heated square cylinder, using a hybrid Navier–Stokes–lattice Boltzmann numerical method
MR Salimi, M Taeibi-Rahni, F Jam
International Journal of Thermal Sciences 91, 59-75, 2015
182015
Design of Physical Configuration of a 10N Monopropellant Hydrazine Thruster
H Karimaei, MR Salimi, H Naseh, E Jokari
Space Science and Technology 12 (1), 13-22, 2019
152019
Pore-scale simulation of fluid flow passing over a porously covered square cylinder located at the middle of a channel, using a hybrid MRT-LBM–FVM approach
MR Salimi, M Taeibi Rahni, F Jam
Theoretical and Computational Fluid Dynamics 29, 171-191, 2015
142015
New lifting relations for estimating LBM distribution functions from corresponding macroscopic quantities, based on equilibrium and non-equilibrium moments
MR Salimi, M Taeibi-Rahni
Journal of Computational Physics 302, 155-175, 2015
132015
Pore-scale modeling of rarefied gas flow in fractal micro-porous media, using lattice Boltzmann method (LBM)
H Rostamzadeh, MR Salimi, M Taeibi-Rahni
Journal of Thermal Analysis and Calorimetry 135, 1931-1942, 2019
112019
Film cooling effectiveness enhancement applying another jet in the upstream neighbor of the main jet-using les approach
MR Salimi, M Ramezanizadeh, M Taeibi-Rahni, R Farhadi-Azar
Journal of Applied Fluid Mechanics 9 (1), 33-42, 2015
92015
Making catalyst and preparing catalyst bed for hydrazine decomposition in Low-thrust monopropellant thrusters
MR Salimi, H Karimaei
Technology in Aerospace Engineering 2 (1), 17-25, 2018
82018
Numerical study of using perforated conical turbulators and added nanoparticles to enhance heat transfer performance in heat exchangers
A Farajollahi, A Mokhtari, M Rostami, K Imani, M Salimi
Scientia Iranica 30 (3), 1027-1038, 2023
72023
Computational investigation of effects of sideinjection geometry on thrust-vectoring performance in a fuel-injected dual throat nozzle
MR Salimi, R Askari, M Hasani
Journal of Applied Fluid Mechanics 15 (4), 1137-1153, 2022
52022
Analysis of misalignment effects on hydrodynamic non-circular journal bearings using three-dimensional lattice boltzmann method
Z Saboohi, S Roofeh, MR Salimi
Iranian Journal of Science and Technology, Transactions A: Science 44, 1739-1751, 2020
52020
Numerical Study of Catalyst Bed Length and Particle Size Effect on the Monopropellant Thruster Specific Impulse and Thrust
MR Salimi
AEROSPACE MECHANICS JOURNAL 16 (15900123), 53-66, 2020
52020
New hybrid finite volume-thermal lattice Boltzmann method, based on multi relaxation time collision operator
MR Salimi, E Alizadeh-Seresht, M Taeibi-Rahni
International Journal of Heat and Mass Transfer 138, 1281-1294, 2019
52019
Numerical simulation of film cooling around a gas turbine blade via partially averaged navier-stokes approach (PANS)
NH Vajargah, MR Salimi, M Taeibi-Rahni
Mechanical Engineering 48 (3), 2016
42016
Aerodynamic Analysis of Cargo Speed Reduction Parachutes using Numerical simulation
MR Salimi, AH Farajolahi, AH Mohseni Kafshgar Kolahi, M Rostami
Fluid Mechanics & Aerodynamics 10 (2), 1-17, 2022
32022
Numerical Analysis of Loads and Stresses Exerting on a Ribbon Type Parachute
M Salimi, A Farajollahi, A Mohsenikafshgarkolaei, M Ebrahimi, M Ayoobi
Journal of Advanced Defense Science & Technology 13 (4), 271-282, 2023
22023
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