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

Related Journals