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 290,538
PDF Download 135,928
View Per Article 830.11
PDF Download Per Article 388.37
 
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
  • Quadrotor
  • Helicopter
  • Extended Kalman Filter
  • Particle Swarm Optimization (PSO)
  • Cylindrical Shell
  • Deep Learning
  • Two-phase flow
  • Integrated guidance and control
  • Fuzzy logic
  • Finite element method
  • Lyapunov Stability
  • Optimal guidance
  • GPS
  • Simulation
  • Flight Dynamics
  • guidance
  • aerodynamic coefficients
  • heat transfer
  • Buckling
  • Flight simulation
  • Nonlinear
  • Direct Collocation
  • Trajectory Tracking
  • Mathematical Modeling
  • Vortex-induced vibration
  • Adaptive control
  • Compressor
  • Aerodynamic
  • Winglet
  • constrained optimization
  • Piezoelectric
  • Aircraft
  • Design of Experiment (DoE)
  • Dynamic Modeling
  • Multidisciplinary design optimization
  • Post-buckling
  • CubeSat
  • the characteristic curve
  • Dielectric Barrier Discharge
  • Porous material
  • launcher
  • Attitude control
  • Large Eddy Simulation
  • Robust predictive control
  • Sliding mode control
  • delta wing
  • Iran
  • Computational Fluid Dynamics
  • EKF
  • Aluminum matrix composite
  • Spacecraft attitude control
  • Boundary element method (BEM)
  • Subsonic
  • Transition Flight
  • attitude estimation
  • Central composite design
  • Radiation
  • Flow Separation
  • Integrated Navigation
  • Reliability
  • Preload
  • Uncertainty
  • Seeker Noise
  • “System Identification”
  • Strouhal number
  • Bluff Body
  • Dynamic Response
  • Miss Distance Analysis
  • Combustion chamber
  • Centrifugal pump
  • UAV
  • B-spline curves
  • Pressure distribution
  • rotor
  • maneuverability
  • Porous media
  • Thermal buckling
  • Robust Control
  • Experimental Aerodynamics
  • Epoxy
  • PSO algorithm
  • Gear train
  • PID Controller
  • Flutter
  • Trajectory Optimization
  • Error compensation
  • Three-body problem
  • Unmanned aerial vehicles
  • Optimization layout gears
  • Droplet
  • plasma actuator
  • Parameter optimization
  • Flow control
  • Aeroelasticity
  • Dynamic Inversion
  • Morphing wing
  • Quadrotor UAV
  • Composites
  • Weight/volume optimization
  • Semi-elliptical crack
  • Neural Network
  • Non-gray gas
  • Bezier Curve
  • Lift
  • Solar Sail Assembly
  • Shell and tube heat exchanger
  • Ducted Fan
  • CNT
  • surge
  • Damped natural frequencies
  • Parts configuration
  • Gas Generator
  • Booster Landing
  • Interaction Force
  • Air Accident
  • shock interactions
  • Ballistic
  • point loads
  • Turbulence
  • Force Measurement
  • Matrix Crack
  • Boltzmann equation
  • Drag and lift coefficient
  • Dynamic analysis
  • Gimballed IMU
  • Springback
  • Particle Swarm Optimization
  • flutter index
  • Coupling of Attitude and Orbital Dynamics
  • Delamination
  • Vacuum Chamber
  • ............................
  • tandem spheres
  • chemical kinetics
  • Visual measurement method
  • “Self-tuning Regulators”
  • Multiaxial fatigue
  • GPS Spoofing
  • “spacecraft”
  • 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
  • Lattice Boltzmann equation
  • Formation flight
  • Aerodynamic configuration
  • Asteroid
  • Inverse simulation
  • Feedback linearization
  • Polymer nanocomposite
  • Premixed Flames
  • Clear air turbulence
  • second order sliding mode control
  • Flow interference
  • atomization
  • Self Alignment
  • Adaptive Mutation
  • stiffness effects
  • Derived Gas Turbine
  • SST K-??turbulence model
  • 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
  • GENEX guidance
  • discrete element method
  • Cantilever cylindrical thick shell
  • composite plates
  • Type2 fuzzy logic
  • cold flow simulation
  • Fiber Matrix Debonding
  • Feedback-linearization
  • Rotor overlap sweep
  • Sensitivity analysis
  • Vibration Analysis
  • winding pattern

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