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

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