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 15-24

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

Numerical Comparison of Film Cooling Methods Effectiveness in a Ramjet Combustor

Pages 51-67

Sajjad Ranjbar, Mohammad Mehdi Doustdar, Kazem Delsoz

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

Pages 83-103

Mohsen Naderi, Mohammad Vajdi, Mehran Abdolalipouradl, Farzad Mohammadkhani

Keywords Cloud

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

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