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

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

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

Mohsen Naderi, Mohammad Vajdi, Mehran Abdolalipouradl, Farzad Mohammadkhani

Keywords Cloud

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

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