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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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