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 13, Issue 2 - Serial Number 34, November 2024, Pages 1-172 (Autumn and winter) 

Experimental study of the effect of Hartmann-Sprenger resonance tube end flow on tube heating performance

Pages 99-111

amirhamzeh farajollahi, Mohsen Rostami, Ehsan Dadkhah, Mostafa mohammadalizadeh Gorji

Calculation of Amphibian Floating Drag under the Effect of Sea Waves Using Computational Fluid Dynamics

Pages 113-124

saleh amini, Mahmoud Rostami Varnousfaaderani, Mojtaba Dehghan Manshadi, Hossein Norouzi

Keywords Cloud

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

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