International Journal of Aerospace Engineering
1.131
Current Impact Factor
1.131
Current Impact Factor
111
Days
Average time from submission to acceptance
43
Days
Average time from acceptance to publication
Most Viewed Articles
| Sandwich structured composites for aeronautics - methods of manufacturing affecting some mechanical properties | 4,413 |
| Conceptual design of an unmanned fixed-wing aerial vehicle based on alternative energy | 3,894 |
| Dynamic Rocker-Bogie: Kinematical Analysis in a High-Speed Traversal Stability Enhancement | 3,472 |
| Study on Flight Performance of Propeller-Driven UAV | 3,425 |
| Aircraft Gas Turbine Engine Health Monitoring System by Real Flight Data | 3,264 |
| Improving aileron effectiveness based on changing the position of aileron connectors | 2,661 |
| Processing Technology Based on Radar Signal Design and Classification | 2,589 |
| Autoclaves for Aerospace Applications: Issues and Challenges | 2,451 |
| Re-Engineering Aircraft Structural Life Prediction Using a Digital Twin | 2,324 |
| The effect of damping coefficient, spring coefficient and mass ratio on the power extraction performance of a semi-active flapping wing | 2,238 |
Most Viewed Special Issue Articles
| Towards the thousandth CubeSat: a statistical overview | 3,697 |
| High-Resolution Image and Video CubeSat (HiREV): Development of Space Technology Test Platform using a Low-Cost CubeSat Platform | 3,627 |
| Design and Implementation of 3U Cubesat Platform Architecture | 3,584 |
| Design, analysis, optimization, manufacturing and testing of a 2U Cubesat | 2,980 |
| Approaches to Low Fuel Regression Rate in Hybrid Rocket Engines | 1,905 |
| Attitude Analysis of Small Satellites using Model-Based Simulation | 1,810 |
| Visual Inspection of Aircraft Surface Using Teleoperated Reconfigurable Climbing Robot and Enhanced Deep Learning Technique | 1,385 |
| Modular design of RF front end for a nano-satellite communication subsystem tile using low cost commercial components | 1,191 |
| AOCS requirements and practical limitations for high speed communications on small satellites | 1,094 |
| Burning Characteristics of Ammonium Nitrate-based Composite Propellants with a Hydroxyl-terminated Polybutadiene/Polytetrahydrofuran-blend Binder | 892 |
