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

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