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

Related Journals