Journal of Aerospace Science and Technology

Journal of Aerospace Science and Technology

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Number of Volumes 19
Number of Issues 45
Number of Articles 350
Number of Contributors 591
Article View 292,297
PDF Download 136,941
View Per Article 835.13
PDF Download Per Article 391.26
 
Accepted Submissions 383
Acceptance Rate 58
Time to Accept (Days) 211
Number of Indexing Databases 9
Number of Reviewers 605

 

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.

 

Current Issue: Volume 18, Issue 2, 2025 

Keywords Cloud

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

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