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) 

Keywords Cloud

  • Numerical Simulation
  • Aerodynamic Coefficients
  • Magnetic Field
  • Wind Tunnel
  • Computational Fluid Dynamics
  • Drag Coefficient
  • Heat Transfer
  • Flow Separation
  • CFD
  • Turbulent Flow
  • Nanofluid
  • Strouhal Number
  • Lattice Boltzmann Method
  • Numerical Solution
  • Optimization
  • Vortex
  • Mixed Convection
  • Cavitation
  • Flow Control
  • Porous Media
  • Two-Phase Flow
  • Drag Force
  • Combustion Chamber
  • Stability
  • Turbocharger
  • Drag
  • Cavity
  • NACA0012 Airfoil
  • Hybrid Nanofluid
  • Lattice Fin
  • Computational Fluid Dynamics (CFD)
  • Natural Convection
  • Turbine Blade
  • Turbofan Engine
  • Airfoil
  • Efficiency
  • Axial Compressor
  • Conjugate Heat Transfer
  • Numerical Analysis
  • Unsteady Flow
  • Internal Combustion Engine
  • underwater vehicle speedometry
  • Response Surface Method
  • Nano Fluid
  • Plasma
  • Viscosity
  • Wind Turbine
  • Large eddy simulation (LES)
  • Plasma Actuator
  • Nusselt Number
  • Reliability
  • aerodynamic efficiency
  • Magnetohydrodynamic
  • Turbine
  • wind tunnel testing
  • Porous Medium
  • Inverse Design Problem
  • Cylinder
  • Fuel Spray
  • computational fluid dynamic
  • Numerical study
  • Hot Wire Anemometry
  • Aerodynamic Performance
  • Bubble Dynamics
  • Blood Flow
  • Numerical investigation
  • differential pressure sensor
  • desalination
  • Reynolds Number
  • free-end cylinder
  • Free Surface
  • Experimental Test
  • Numerical modeling
  • Large Eddy Simulation Approach
  • Drag Reduction
  • Non Uniform Magnetic Field
  • Turboprop Engine
  • thrust force
  • Nanoparticles
  • Geometric Shape
  • One Dimensional Modeling
  • Aerodynamic Coefficient
  • Microbubble
  • flying wing
  • Finite Difference
  • Mach number
  • 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
  • Aerodynamics
  • Flash cycle
  • Winged bombletautorotation
  • Aerodynamics Efficiency
  • Compressible flow
  • Flow Turbulence Intensity
  • Cylindrical Model
  • Three-dimensional Euler Equations
  • Blade
  • Liquid Film
  • wind turbine blade
  • sound absorber
  • Aerodynamics Coefficient of Missile
  • Nonlinear saturation function
  • Compressor
  • slat
  • Absorption Refrigeration
  • Plunge Airfoil
  • Droplet Evaporation
  • Solar irradiance
  • Fractal Interpolation
  • Two-Dimensional Simulation
  • Drop Height
  • \"Transonic\"
  • Finite Element
  • DTMB4119 Propeller
  • Pulsing Illuminator
  • : Detonation Combustion Wave
  • Accuracy and Stability of Solution
  • air gap
  • 5-Hole Probe
  • Premixed flame
  • Radiation Heat Transfer
  • Heat source
  • longitudinal instability
  • Efficient methods
  • operational parameters
  • Exergy Analysis
  • Uncertainty quantification
  • Gappy points
  • Natural and Forced Convections
  • Optimized nanoparticles
  • solar cell efficiency
  • Aeroballistic test
  • Fuel system
  • Ag-Water
  • Thermodynamic modeling
  • Lifting control surfaces of the wing
  • lipid shedding
  • Induced Vibrations
  • Diffusion Ratio
  • : Viscous Shock Layer and Similarity Boundary Layer
  • : Cavitation
  • Non-linear Equations
  • Radiator Tube Arrangement
  • Rotating
  • Holes Distribution
  • Transonic Wind Tunnel
  • Two Phases Stream
  • Laboratory study
  • Cogeneration
  • Stability Coefficients
  • Stabilizer Parachute
  • Microfluidic
  • Annular Tube Heat Exchanger
  • Entropy Production
  • Air inlet velocity
  • Mixed-Convection
  • Submerged Inlet
  • Flow Visualization
  • Barotropic Vorticity Equation
  • natural gas transmission
  • chord and width
  • Heat Shield
  • Film Cooling
  • Phase Changes
  • Modeling
  • bulk-membrane combined wing
  • Film Cooling Effectiveness
  • Kalman Filter
  • Deep Neural Network
  • Re-entry Projectile
  • Flame holder
  • mirrored airfoils
  • Forebody Distance
  • Axisymmetric
  • 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
  • Internal Flow
  • Experimental Jet Breakup
  • hydrofoil

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