>
Fa
  |  
Ar
  |  
En
  
journal of aerospace science and technology
  
سال:2020 - دوره:13 - شماره:1
  
 
Calculation of Nonlinear Normal Modes Using EPFM Method
- صفحه:57-65
  
 
Designing a Fault-Tolerant Control System for the Boeing 747
- صفحه:1-9
  
 
Experimental Comparison of Thrust Performance of Two Low and Medium-Speed Motors by Wind Tunnels and Obtaining the Flight Time of a Specific Drone
- صفحه:11-17
  
 
Experimental Investigation of The Geometric Properties of Different Rotor Blades for Controlling the Wingtip Vortex
- صفحه:89-98
  
 
Growth and Collapse of a Cavitation Bubble Inside a Rigid Cylinder: Effect of Membrane Tension
- صفحه:67-76
  
 
Modeling of 9 Degrees of Parafoil Freedom through Transverse Displacement of Cargo Weight
- صفحه:27-38
  
 
Neural Network Backstepping control of a reentry vehicle in the presence of uncertainties
- صفحه:77-81
  
 
Numerical Investigation of Aerodynamic Effects of Geometry and Sensor Distance on a Spherical Projectile
- صفحه:39-47
  
 
Numerical Study of Changes in Length-to- Diameter Ratio of a Cylindrical Diffuser, Used in a Vacuum Test Stand
- صفحه:18-25
  
 
Optimal Flight Trajectory Planning using Improved Evolutionary Method for UCAV Navigation in 3D Constrained Environments
- صفحه:83-89
  
 
Optimal Guidance of a Reentry Vehicle Based on Online Trajectory Optimization
- صفحه:99-110
  
 
Simulation and Examination of Flow Characteristics of the Butterfly Valve
- صفحه:49-56
Copyright 2023
Islamic World Science Citation Center
All Rights Reserved