Journal of Aerospace Science and Technology

Journal of Aerospace Science and Technology

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Number of Volumes 20
Number of Issues 46
Number of Articles 357
Number of Contributors 601
Article View 317,633
PDF Download 172,548
View Per Article 889.73
PDF Download Per Article 483.33
 
Accepted Submissions 388
Acceptance Rate 58
Time to Accept (Days) 212
Number of Indexing Databases 9
Number of Reviewers 635

 

I am pleased to introduce this new journal in aerospace science and technology. Journal of Aerospace Science and Technology is an open-access, double-blind, peer-reviewed semiannual publication published by the Iranian Aerospace Society. As we understand, there is little or no forum in this field with an international scope in the region of central and west Asia. Therefore we strongly believe that it will make it possible in the region and in the whole world for better communication among scientists and researchers in aeronautical and astronautical sciences and technologies, and also in all related fields as aerodynamics and fluid mechanics, thermodynamics, and propulsion, combustion and heat transfer, dynamics and control, flight mechanics, design, structures and vibration, aviation management, etc.  To start a new submission, please first read the Guide for Authors page for detailed information about manuscript format, style, and other requirements. Manuscript submission, refereeing, and publishing are completely free of charge. New manuscripts should be submitted online by the corresponding author through the website after registration. This journal follows the Committee on Publication Ethics (COPE) and complies with the highest ethical standards following ethical laws. (Read more about this journal...)


It is necessary for authors to register a unique ORCID research ID in this publication. 
It is necessary to enter the exact details of the department, faculty, university, province, country, and ORCID research ID in the authors' affiliation section when registering the article.

Please note that the new email address for the  journal is as follows:
 jastanjoman@gmail.com
Publication order: Semiannual
Language: English
Rank in the Ministry of Science of IRAN: A
Type publication: Online
Type of Access: Open access (full text)

All articles published in the journal are in a state of open access for the public to study or scientific exploit following the principles of research and correct citation.

 

Keywords Cloud

  • optimization
  • CFD
  • Wind tunnel
  • Finite Element
  • Genetic Algorithm
  • Quadrotor
  • numerical simulation
  • Kalman Filter
  • Helicopter
  • Simulation
  • Particle Swarm Optimization (PSO)
  • Finite element method
  • Lyapunov Stability
  • Cylindrical Shell
  • Integrated guidance and control
  • Flight Dynamics
  • Optimal guidance
  • heat transfer
  • Deep Learning
  • GPS
  • guidance
  • Artificial intelligence
  • Two-phase flow
  • aerodynamic coefficients
  • Extended Kalman Filter
  • Fuzzy logic
  • Spacecraft attitude control
  • Buckling
  • Direct Collocation
  • Dynamic Inversion
  • Composites
  • Aircraft
  • attitude estimation
  • delta wing
  • Combustion chamber
  • Miss Distance Analysis
  • Computational Fluid Dynamics
  • B-spline curves
  • Robust predictive control
  • Large Eddy Simulation
  • Vortex-induced vibration
  • Epoxy
  • Design of Experiment (DoE)
  • Gear train
  • Transition Flight
  • the characteristic curve
  • Subsonic
  • Boundary element method (BEM)
  • Aerodynamic
  • Aeroelasticity
  • Post-buckling
  • Adaptive control
  • Compressor
  • Uncertainty
  • PSO algorithm
  • Nonlinear
  • Trajectory Tracking
  • Flow control
  • Three-body problem
  • Thermal buckling
  • Dielectric Barrier Discharge
  • EKF
  • maneuverability
  • Weight/volume optimization
  • Winglet
  • Experimental Aerodynamics
  • CubeSat
  • Central composite design
  • Radiation
  • Flow Separation
  • Sliding mode control
  • Bluff Body
  • Dynamic Response
  • Preload
  • Seeker Noise
  • Fatigue life
  • Centrifugal pump
  • UAV
  • Reliability
  • Piezoelectric
  • Pressure distribution
  • constrained optimization
  • Porous media
  • Porous material
  • launcher
  • Robust Control
  • Strouhal number
  • Multidisciplinary design optimization
  • PID Controller
  • Dynamic Modeling
  • Integrated Navigation
  • Multi-Objective Optimization
  • “System Identification”
  • rotor
  • Flutter
  • Trajectory Optimization
  • Error compensation
  • Unmanned aerial vehicles
  • Optimization layout gears
  • Droplet
  • Aluminum matrix composite
  • Attitude control
  • Parameter optimization
  • Flight simulation
  • Quadrotor UAV
  • Morphing wing
  • Mathematical Modeling
  • Neural Network
  • plasma actuator
  • Iran
  • Semi-elliptical crack
  • Shell and tube heat exchanger
  • Bezier Curve
  • Ducted Fan
  • Solar Sail Assembly
  • standardization
  • Parts configuration
  • Boltzmann equation
  • Delamination
  • Damped natural frequencies
  • Gas Generator
  • surge
  • Booster Landing
  • Interaction Force
  • Air Accident
  • shock interactions
  • Drag and lift coefficient
  • Gimballed IMU
  • Force Measurement
  • Dynamic analysis
  • Matrix Crack
  • Coupling of Attitude and Orbital Dynamics
  • Particle Swarm Optimization
  • Springback
  • flutter index
  • ............................
  • tandem spheres
  • chemical kinetics
  • GPS Spoofing
  • Vacuum Chamber
  • Visual measurement method
  • “spacecraft”
  • Multiaxial fatigue
  • “Self-tuning Regulators”
  • gray wolf optimization algorithm
  • Magnetometer calibration
  • the critical cavitation number
  • Transonic
  • axial-flow compressor
  • robustness
  • Airplane wing
  • De-orbiting
  • Optimum parameters
  • Turbulence model
  • CFD video technique
  • Gurney flap
  • Modified Predictive Kalman Filter (MPKF)
  • hybrid wick
  • Inverse simulation
  • Lattice Boltzmann equation
  • Formation flight
  • Asteroid
  • Clear air turbulence
  • Aerodynamic configuration
  • second order sliding mode control
  • Adaptive Mutation
  • multi-agent systems
  • Feedback linearization
  • Polymer nanocomposite
  • Flow interference
  • atomization
  • Self Alignment
  • stiffness effects
  • SST K-??turbulence model
  • Hingeless
  • gas-dynamics
  • Shape Optimization
  • apparent mass
  • High Aspect Ratio Wings
  • GENEX guidance
  • Cantilever cylindrical thick shell
  • Galloping
  • Wing Rock Phenomenon
  • Derived Gas Turbine
  • Unsteady Aerodynamic Model
  • Pilot-Induced Oscillation
  • Actuator Fault
  • robust flight control
  • Multi-Input - Multi-Output Controller
  • Orbit Determination
  • Robot- Flexible Link- Finite Element- Maximum Allowable Dynamic Load
  • Boundary Layer
  • Premixed Flames
  • discrete element method
  • high speed and high altitude target
  • Triangular
  • Type2 fuzzy logic
  • cold flow simulation
  • Fiber Matrix Debonding
  • Mixed convection

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