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, Pages 1-182 (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
  • Computational Fluid Dynamics
  • Drag Coefficient
  • Magnetic Field
  • Wind Tunnel
  • Aerodynamic Coefficients
  • Heat Transfer
  • Turbulent Flow
  • Lattice Boltzmann Method
  • Flow Separation
  • Flow Control
  • CFD
  • Nanofluid
  • Combustion Chamber
  • Strouhal Number
  • Two-Phase Flow
  • Stability
  • Vortex
  • Porous Media
  • Cavitation
  • Optimization
  • Numerical Solution
  • Drag Force
  • Airfoil
  • Mixed Convection
  • Natural Convection
  • Conjugate Heat Transfer
  • Turbocharger
  • Turbofan Engine
  • Experimental Test
  • Computational Fluid Dynamics (CFD)
  • Numerical Analysis
  • NACA0012 Airfoil
  • Axial Compressor
  • Lattice Fin
  • Turbine Blade
  • Drag Reduction
  • Aerodynamics
  • Efficiency
  • Drag
  • Hybrid Nanofluid
  • Cavity
  • Tube
  • Ramjet Engine
  • Flow Field
  • Supersonic Flow
  • Shock Waves
  • Nusselt Number
  • Free Surface
  • Geometric Shape
  • aerodynamic efficiency
  • differential pressure sensor
  • Hydrodynamic Coefficients
  • Response Surface Method
  • aerospike
  • Turbine
  • Porous Medium
  • Internal Combustion Engine
  • Finite Difference
  • Mach number
  • Cylinder
  • Inverse Design Problem
  • Aerodynamic Coefficient
  • Microbubble
  • Fuel Spray
  • Numerical investigation
  • Aerodynamic Performance
  • Nanoparticles
  • One Dimensional Modeling
  • Turboprop Engine
  • Vortex generator
  • Large eddy simulation (LES)
  • Numerical modeling
  • free-end cylinder
  • Reliability
  • Wind Turbine
  • Reynolds Number
  • Blood Flow
  • Viscosity
  • underwater vehicle speedometry
  • computational fluid dynamic
  • Numerical study
  • lift coefficient
  • Hot Wire Anemometry
  • blunt noses
  • Film Cooling
  • aerodynamic optimization
  • Film Cooling Effectiveness
  • Bubble Dynamics
  • Non Uniform Magnetic Field
  • Supersonic Wind Tunnel
  • Plasma
  • Plasma Actuator
  • Range
  • Magnetohydrodynamic
  • Baffle
  • Large Eddy Simulation Approach
  • Ice Accretion
  • Ignition Advance
  • Dynamic stall
  • Turbulence Modeling
  • Hypersonic Wind Tunnel
  • 3D Simulation
  • Micro-turbofan engine
  • Lattice Boltzmann Method (LBM)
  • thrust force
  • Nano Fluid
  • Flash cycle
  • Winged bombletautorotation
  • Aerodynamics Efficiency
  • Compressible flow
  • Plunge Airfoil
  • Cylindrical Model
  • Three-dimensional Euler Equations
  • Absorption Refrigeration
  • Blade
  • slat
  • sound absorber
  • Liquid Film
  • Droplet Evaporation
  • Flow Turbulence Intensity
  • Fractal Interpolation
  • Two-Dimensional Simulation
  • Drop Height
  • \"Transonic\"
  • Finite Element
  • wind turbine blade
  • membrane Combined Wing
  • Aerodynamics Coefficient of Missile
  • Solar Energy Hybrid System Desalination Thermoelectric Photovoltaic
  • Accuracy and Stability of Solution
  • Unsteady Flow
  • Compressor
  • Solar irradiance
  • : Detonation Combustion Wave
  • air gap
  • Premixed flame
  • Nonlinear saturation function
  • Radiation Heat Transfer
  • Heat source
  • longitudinal instability
  • Heatsink Arrangement Cross
  • Efficient methods
  • operational parameters
  • Exergy Analysis
  • Uncertainty quantification
  • Gappy points
  • Natural and Forced Convections
  • Optimized nanoparticles
  • solar cell efficiency
  • Aeroballistic test
  • Enhancement of Efficiency
  • 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
  • Thermal (PV/T
  • Laboratory study
  • Two Phases Stream
  • Flame holder
  • Stabilizer Parachute
  • Microfluidic
  • Air inlet velocity
  • Modeling
  • Fueled Gas Turbine Cogeneration Energy and Exergy Efficiency
  • Submerged Inlet
  • Heat Shield
  • chord and width
  • Phase Changes
  • Flow Visualization
  • Barotropic Vorticity Equation
  • Mixed-Convection
  • Entropy Production
  • natural gas transmission
  • Deep Neural Network
  • Annular Tube Heat Exchanger
  • Stability Coefficients
  • Forebody Distance
  • Axisymmetric
  • microchannel
  • Sensitivity
  • Radial Compressor
  • Aerospace Vehicles
  • Inclined backward-facing step
  • Bubble Injection
  • Hydraulic oil
  • Cell culture
  • Performance Modeling
  • Zwart
  • Re-entry Projectile
  • Experimental Jet Breakup

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