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journal of aerospace science and technology
  
سال:2021 - دوره:14 - شماره:1
  
 
A Study on Lean, Sweep and Chord Length Effects on Aerodynamic Performance of Axial Fan of a High-bypass ratio Turbofan Engine
- صفحه:45-55
  
 
A theoretical analysis of the influence of winding patterns on buckling load of filament wound composite pipes
- صفحه:83-90
  
 
Analysis of Composite Lattice Cylindrical Shells Under Transient Dynamic Loading
- صفحه:31-44
  
 
Critical Cavitation Number Determination of a High-speed Centrifugal Pump by Numerical Simulation of a Two-phase Flow
- صفحه:91-102
  
 
Design of Multi-Input Multi-Output Controller for an Unmanned Aerial Vehicle by Eigenstructure Assignment Method
- صفحه:117-127
  
 
Experimental Investigation of using Plasma Actuators as Virtual Gurney Flap
- صفحه:103-110
  
 
Investigating the Effect of Different Winglet Cant Angles on a Supercritical Wing Aerodynamic Efficiency at Lower Reynolds numbers
- صفحه:106-112
  
 
Investigation of fin changes effects on aerodynamic performance of airship
- صفحه:1-10
  
 
Model Predictive Fault Tolerant Control of Two-Tethered Satellite System
- صفحه:128-142
  
 
Model Reference Adaptive Control Using a New Adaptation Law Based on Power-Series Quadratic Lyapunov Functions for the Single Degree of Freedom Wing Rock Phenomenon
- صفحه:11-25
  
 
Optimal decision making in designing an Earth observation mission with considering the technical challenges of the platform and the impossibility of injection into the sunsynchronous orbit
- صفحه:73-83
  
 
Semi-analytical solution of a threedimensional transient response of a functionally graded annular plate with a piezoelectric layer
- صفحه:56-72
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