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 291,672
PDF Download 136,506
View Per Article 833.35
PDF Download Per Article 390.02
 
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
  • Finite Element
  • Genetic Algorithm
  • Kalman Filter
  • numerical simulation
  • Helicopter
  • Quadrotor
  • Extended Kalman Filter
  • Cylindrical Shell
  • Optimal guidance
  • Lyapunov Stability
  • Flight Dynamics
  • Two-phase flow
  • Integrated guidance and control
  • Deep Learning
  • Finite element method
  • Particle Swarm Optimization (PSO)
  • heat transfer
  • aerodynamic coefficients
  • Fuzzy logic
  • guidance
  • GPS
  • Simulation
  • Buckling
  • Flight simulation
  • Nonlinear
  • Direct Collocation
  • Trajectory Tracking
  • Dynamic Inversion
  • Vortex-induced vibration
  • Adaptive control
  • Compressor
  • Attitude control
  • Winglet
  • constrained optimization
  • Piezoelectric
  • Aircraft
  • Design of Experiment (DoE)
  • Dynamic Modeling
  • PSO algorithm
  • Post-buckling
  • CubeSat
  • Epoxy
  • Dielectric Barrier Discharge
  • the characteristic curve
  • Porous material
  • launcher
  • Aeroelasticity
  • Miss Distance Analysis
  • Sliding mode control
  • Iran
  • Robust predictive control
  • Computational Fluid Dynamics
  • EKF
  • Aluminum matrix composite
  • Spacecraft attitude control
  • Boundary element method (BEM)
  • Subsonic
  • Transition Flight
  • attitude estimation
  • Central composite design
  • Large Eddy Simulation
  • Flow Separation
  • Integrated Navigation
  • Reliability
  • Preload
  • Strouhal number
  • Seeker Noise
  • “System Identification”
  • Neural Network
  • Bluff Body
  • Dynamic Response
  • Combustion chamber
  • Radiation
  • Centrifugal pump
  • UAV
  • B-spline curves
  • Pressure distribution
  • rotor
  • maneuverability
  • Porous media
  • Thermal buckling
  • Robust Control
  • Experimental Aerodynamics
  • Multidisciplinary design optimization
  • PID Controller
  • Gear train
  • Flutter
  • Trajectory Optimization
  • Error compensation
  • Unmanned aerial vehicles
  • Three-body problem
  • Optimization layout gears
  • Droplet
  • plasma actuator
  • Parameter optimization
  • Flow control
  • Quadrotor UAV
  • Morphing wing
  • Aerodynamic
  • Mathematical Modeling
  • Weight/volume optimization
  • Composites
  • Semi-elliptical crack
  • delta wing
  • Uncertainty
  • Non-gray gas
  • Bezier Curve
  • Lift
  • Solar Sail Assembly
  • Shell and tube heat exchanger
  • Ducted Fan
  • CNT
  • Gas Generator
  • Parts configuration
  • Damped natural frequencies
  • 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
  • De-orbiting
  • Turbulence model
  • CFD video technique
  • Optimum parameters
  • Gurney flap
  • Modified Predictive Kalman Filter (MPKF)
  • hybrid wick
  • Type2 fuzzy logic
  • Formation flight
  • Lattice Boltzmann equation
  • 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
  • composite plates
  • cold flow simulation
  • Fiber Matrix Debonding
  • Feedback-linearization
  • Rotor overlap sweep
  • Vibration Analysis
  • Sensitivity analysis
  • gas-dynamics

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