Fluid Mechanics & Aerodynamics

Fluid Mechanics & Aerodynamics

" Fluid Mechanics and Aerodynamics " Journal, based on the regulation of scientific journals of the Ministry of Science, Research and Technology, in the assessment of 1402 (2023) has been ranked "B".

According to the latest review and ranking of the country's scientific journals in the Islamic World Science Citation Database (ISC), the scientific journal of Fluid Mechanics and Aerodynamics has been ranked Q3 in terms of quality.

Information of Journal 


  • Start of journal: 2012
  • Credit of the journal: Scientific-Research
  • Type of articles to be published: Research, promotional
  • Format: Print and Online
  • Frequency: Semiannual
  • Language: Persian; including English abstracts
  • Coverage: Fluid Mechanics and Aerodynamics 
  • Type of Peer-Review: Double Blind Peer Review; two reviewers
  • Average Review Time: 3 months Maximum
  • Manual of style of the journal:  Vancouver
  • Contact E-mail: sayalat@ihu.ac.ir
  • Article Processing, Publishing and judging Charges: Free 
  • Type of License: CC BY
  • Type of Access: Open Access (OA) 

Hints:

1. Respected authors are requested to follow the format of the Jornal in order to speed up the review and judging process.

2. Respecting the rules of ethics in journals, this journal is subject to the rules of the Committee on Ethics in journal (COPE) and follows the executive regulations of the Law on Prevention and combating fraud in Scientific Works.

3. In order to prevent plagiarism, it is necessary to send a report to Samim Noor text matching system or Irandak matching system at the time of submitting the article.

4. Also, please, when submitting the article (commitment form), (authors conflict of interest form) and form (authors' Profile) must be signed by all authors and uploaded to the system.

Note: Make sure to print out the commitment and conflict of interest file and sign it manually, and then upload the scanned file.

In addition, the file must be in PDF format or in the form of a photo.

5. Audience: The audience of this Journal is made up of professors, academic faculty members of universities, experts in mechanics and related fields.

Current Issue: Volume 14, Issue 2 - Serial Number 36, February 2026 (Autumn and Winter) 

Experimental Parametric Study of Factors Affecting the Negative Corona Plasma Propulsion System

Pages 13-25

Seyed Abolfazl Mousavi, Farshad Pazooki, Seyed Hossein Sadati, Rouhollah Khoshkhoo

Using Taguchi Method for Optimization of a Biogas-Fueled Gas Turbine-Based Cogeneration System

Pages 85-99

Mohsen Naderi, Mohammad Vajdi, Mehran Abdolalipouradl, Farzad Mohammadkhani

Keywords Cloud

  • Numerical Simulation
  • Magnetic Field
  • Wind Tunnel
  • Computational Fluid Dynamics
  • Drag Coefficient
  • Aerodynamic Coefficients
  • Heat Transfer
  • Turbulent Flow
  • Flow Separation
  • Strouhal Number
  • Combustion Chamber
  • Lattice Boltzmann Method
  • Nanofluid
  • CFD
  • Flow Control
  • Airfoil
  • Vortex
  • Stability
  • Mixed Convection
  • Optimization
  • Numerical Solution
  • Porous Media
  • Drag Force
  • Cavitation
  • Two-Phase Flow
  • Conjugate Heat Transfer
  • Drag Reduction
  • Cavity
  • Efficiency
  • Natural Convection
  • Computational Fluid Dynamics (CFD)
  • Numerical Analysis
  • Turbocharger
  • Turbofan Engine
  • Turbine Blade
  • Lattice Fin
  • Hybrid Nanofluid
  • Axial Compressor
  • Aerodynamics
  • NACA0012 Airfoil
  • Drag
  • Internal Combustion Engine
  • Tube
  • Response Surface Method
  • Nano Fluid
  • underwater vehicle speedometry
  • Ice Accretion
  • Large eddy simulation (LES)
  • Turboprop Engine
  • Hot Wire Anemometry
  • Reynolds Number
  • Non Uniform Magnetic Field
  • Supersonic Wind Tunnel
  • Ramjet Engine
  • Microbubble
  • Porous Medium
  • Film Cooling
  • Mach number
  • Inverse Design Problem
  • Film Cooling Effectiveness
  • Aerodynamic Coefficient
  • computational fluid dynamic
  • One Dimensional Modeling
  • Cylinder
  • Geometric Shape
  • Numerical investigation
  • Blood Flow
  • Experimental Test
  • Numerical modeling
  • differential pressure sensor
  • Reliability
  • Viscosity
  • Nusselt Number
  • free-end cylinder
  • Wind Turbine
  • Free Surface
  • Bubble Dynamics
  • thrust force
  • aerodynamic efficiency
  • Numerical study
  • Fuel Spray
  • Turbine
  • aerospike
  • blunt noses
  • Plasma Actuator
  • Finite Difference
  • Plasma
  • Large Eddy Simulation Approach
  • Range
  • Magnetohydrodynamic
  • Baffle
  • Lattice Boltzmann Method (LBM)
  • Dynamic stall
  • lift coefficient
  • Ignition Advance
  • Micro-turbofan engine
  • Turbulence Modeling
  • Hypersonic Wind Tunnel
  • 3D Simulation
  • Flow Field
  • Hydrodynamic Coefficients
  • Nanoparticles
  • Aerodynamic Performance
  • Flash cycle
  • Winged bombletautorotation
  • Three-dimensional Euler Equations
  • Compressible flow
  • slat
  • Cylindrical Model
  • wind turbine blade
  • Blade
  • membrane Combined Wing
  • Aerodynamics Coefficient of Missile
  • Liquid Film
  • Compressor
  • Accuracy and Stability of Solution
  • sound absorber
  • Unsteady Flow
  • air gap
  • Absorption Refrigeration
  • Plunge Airfoil
  • Droplet Evaporation
  • Flow Turbulence Intensity
  • Fractal Interpolation
  • Two-Dimensional Simulation
  • Drop Height
  • Premixed flame
  • Solar Energy Hybrid System Desalination Thermoelectric Photovoltaic
  • Solar irradiance
  • : Detonation Combustion Wave
  • Radiation Heat Transfer
  • Nonlinear saturation function
  • longitudinal instability
  • operational parameters
  • Heat source
  • Jet Hole Blockage
  • Exergy Analysis
  • Optimized nanoparticles
  • Efficient methods
  • Natural and Forced Convections
  • Aeroballistic test
  • solar cell efficiency
  • Uncertainty quantification
  • Gappy points
  • Ag-Water
  • Lifting control surfaces of the wing
  • lipid shedding
  • Enhancement of Efficiency
  • Diffusion Ratio
  • Thermodynamic modeling
  • : Viscous Shock Layer and Similarity Boundary Layer
  • Transonic Wind Tunnel
  • Induced Vibrations
  • Thermal (PV/T
  • Cogeneration
  • : Cavitation
  • Microfluidic
  • Radiator Tube Arrangement
  • Length Oscillation
  • Holes Distribution
  • Two Phases Stream
  • Forebody Distance
  • Laboratory study
  • Air inlet velocity
  • Flame holder
  • Stabilizer Parachute
  • Non-linear Equations
  • Flow Visualization
  • Modeling
  • Barotropic Vorticity Equation
  • Heat Shield
  • chord and width
  • Phase Changes
  • wind tunnel testing
  • natural gas transmission
  • Deep Neural Network
  • Re-entry Projectile
  • Submerged Inlet
  • Experimental Jet Breakup
  • mirrored airfoils
  • Mixed-Convection
  • Entropy Production
  • hydrofoil
  • Kalman Filter
  • Annular Tube Heat Exchanger
  • Stability Coefficients
  • Pseudo spectral solver
  • Axisymmetric
  • microchannel
  • Sensitivity
  • Radial Compressor
  • Aerospace Vehicles
  • Inclined backward-facing step
  • Bubble Injection
  • Hydraulic oil
  • Cell culture
  • Performance Modeling
  • Zwart
  • blade outlet angle
  • Calibration

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