Aerospace Mechanics

Aerospace Mechanics

Journal Information


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 Aerospace Mechanics has been ranked Q3 in terms of quality.

This Journal , which is published by the technical and engineering faculty and research institute of Imam Hossein University (AS), under license 3/2910/472 dated 5/26/ 83 of the Ministry of Science, Research and Technology under the title "Aerospace Mechanics" has been published with a scientific-research degree.

This Journal publish the latest achievements of the country's researchers, which are the result of original research and contain new results in the specialized fields of the following five main trends:

  1. Vibration dynamics and control
  2. Solid Mechanics
  3. Propulsion and heat transfer
  4. Manufacturing and Production
  5. Impact mechanics

  • Type of Access: Open Access (OA) 
  • Start of Journal : 2005
  • Credit of the Journal : Scientific-Research
  • Type of articles to be published: Research
  • Format: Print and Online
  • Frequency: Quarterly
  • Language: Persian; including English abstracts
  • Coverage: Theories, Models and Systems Related of Aerospace Mechanics
  • Type of peer-review: Double Blind Peer Review; two reviewers
  • Initial review period: 1 week
  • Average time for review articles: Maximum 20 days
  • Manual of style of the Journal : Vancouver
  • Article Processing, Publishing and judging Charges: Free for review process and Journal
  • Contact E-mail: Havafaza@ihu.ac.ir
  • Cooperation with the association: Scientific Association of High Energy Materials of Iran
  • Type of License: CC BY-NC

Audience: The audience of this Journal is made up of professors, academic faculty members of universities, experts in mechanics and related fields.

Faculty members, researchers, and graduate students are invited to prepare their Persian article according to the article preparation guide and by visiting the Journal website (http://maj.ihu.ac.ir) and registering in it, Send the electronic version of the article to the Journal office.

** Submitted articles must not have been previously published in any Journal .**

  1. Respected authors are requested to follow the format of the Journal 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 Journals  (COPE) and follows the executive regulations of the Law on Prevention and combating fraud in Scientific Works.
  3. All articles sent to this  Journal  are reviewed by plagiarism software. Submitting the report of Samim Noor similarity  check system or Irandak similarity  check system is also necessary at the time of submitting the article. (Link to the guide to the plagiarism detector system)
  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.

Keywords Cloud

  • Numerical Simulation
  • Sliding Mode Control
  • genetic algorithm
  • Natural frequency
  • Optimization
  • Buckling
  • Mechanical Properties
  • Cylindrical Shell
  • Carbon nanotube
  • Robust Control
  • Heat Transfer
  • Inertial Navigation
  • Finite Element
  • Composite
  • Response Surface Methodology
  • Extended State Observer
  • Energy Absorption
  • Stability
  • First order shear deformation theory
  • Piezoelectric
  • Energy harvesting
  • Kalman Filter
  • Functionally graded material
  • Additive manufacturing
  • Gyroscope
  • Repeated loading
  • Multidisciplinary Design Optimization
  • Nonlinear vibrations
  • neural network
  • Sandwich Panel
  • Guidance and Control
  • Turbofan Engine
  • Composite Material
  • free vibration
  • Force Control
  • Finite Element Method
  • Triangular plate
  • differential quadrature method
  • FGM
  • Active vibration control
  • Chattering
  • Model Predictive Control
  • Dynamic loading
  • Extended Kalman Filter
  • Sandwich panels
  • Modal Analysis
  • Elastic foundation
  • Flexible spacecraft
  • Sliding Mode
  • Mixing efficiency
  • PID Controller
  • Nonlinear model predictive control
  • Inertial Navigation System (INS)
  • Shock tube
  • Multi-Objective Optimization
  • Frequency
  • Natural Convection
  • Particle Filter
  • Multi-agent system
  • Tensegrity structure
  • Combustion Chamber
  • Location of Piezoelectric
  • Hybrid nanofluids
  • Composite beam
  • Blast Loading
  • Vibration
  • Trajectory Optimization
  • Mechanical Vibrations
  • Transverse Step
  • Parameter uncertainty
  • Dynamic Analysis
  • Numerical study
  • Molecular dynamics simulations
  • Underactuated system with two degrees of freedom
  • Formation control
  • Twisted Tape
  • Magnetic Field
  • Experimental Investigation
  • finite element analysis
  • Wave Propagation
  • ballistic limit
  • Integrated navigation system
  • instability
  • Stress Intensity Factor
  • Backstepping Control
  • Impact
  • Spacecraft
  • Free vibrations
  • Attitude control
  • Cylindrical shells
  • Non-Newtonian nanofluid
  • Nonlinear Beam
  • ANFIS
  • Fault tolerant control
  • CAD/CAM
  • Low velocity impact
  • Female die
  • Fuzzy Logic
  • Grain refinement
  • Central Composite Design
  • Forced Vibration
  • Nonlinear vibration
  • Shape memory alloy
  • Data Fusion
  • Numerical Method
  • Output Power
  • Rotating beam
  • Finite Element Simulation
  • Fracture Mechanics
  • Signal Processing
  • Analytical modeling
  • Structured and Un-structured uncertainties
  • Graphene
  • Gaseous detonation
  • Piezoelectric layer
  • third order shear deformation theory
  • Fuzzy Controller
  • Nanofluid
  • Terminal Sliding Mode Control
  • Molecular Dynamics
  • Gas Turbine
  • Die forming
  • Underwater explosion
  • Uncertainty
  • Severe plastic deformation
  • Interfacial shear strength
  • Force Density
  • Filament collection speed
  • Turbulent Flow
  • Deflection
  • Continuum approximation method
  • Jump Phenomenon
  • Fuzzy System
  • Image Processing
  • Predictive Control
  • Inertial Navigation System
  • Deep Neural Network
  • Composite lattice structures
  • Vibrations Analysis
  • Inertial Forces
  • Thrust Chamber
  • Corrosion
  • Hybrid Composite Laminate
  • DOM
  • Generalized &alpha
  • Adaptive backstepping approach
  • Flight Control System
  • Optimal Guidance
  • Radial Pressure
  • Combined actuator fault
  • Surface Mounting
  • Frequency Response
  • 3D-Printing
  • Active steering control
  • Linear Model
  • Operational Frequency
  • Dynamic Performance
  • Nondestructive Test
  • Runge Kutta method
  • mold temperature
  • Calorimetry
  • Model uncertainty
  • Nonlinear Programming
  • Piezoelectric Layers
  • Extruder
  • Experimental study
  • simultaneous symmetrical impulsive loading
  • Oblique blast loading
  • Thick Plate
  • Film Cooling
  • Adaptive sliding mode control
  • Porosity
  • Dynamic Optimization
  • Channel
  • Fuzzy C-Means
  • Environmental test
  • critical lane change maneuver
  • Aerodynamic Interference
  • Volumetric radiation
  • Calibration
  • Tube based Model Predictive Control
  • Emergency Condition
  • Fuzzy approximator
  • Attitude Dynamics and Control
  • Failure-based sizing method
  • Flight Performance
  • Monolayer
  • Optimized geometry
  • Friction factor
  • Robust Guidance
  • Cooling flow field
  • Phase transformation models
  • Composites shells
  • Geometrical tolerances
  • Backing Material
  • Pad
  • Frictional work
  • Shaped Charge
  • Cold gas thrusters
  • Bi-Stable Composite Laminates

Related Journals