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   Journal Of Aerospace Science And Technology   
سال:2021 - دوره:14 - شماره:1


  tick  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

  tick  A Theoretical Analysis Of The Influence Of Winding Patterns On Buckling Load Of Filament Wound Composite Pipes - صفحه:83-90

  tick  Analysis Of Composite Lattice Cylindrical Shells Under Transient Dynamic Loading - صفحه:31-44

  tick  Critical Cavitation Number Determination Of A High-Speed Centrifugal Pump By Numerical Simulation Of A Two-Phase Flow - صفحه:91-102

  tick  Design Of Multi-Input Multi-Output Controller For An Unmanned Aerial Vehicle By Eigenstructure Assignment Method - صفحه:117-127

  tick  Experimental Investigation Of Using Plasma Actuators As Virtual Gurney Flap - صفحه:103-110

  tick  Investigating The Effect Of Different Winglet Cant Angles On A Supercritical Wing Aerodynamic Efficiency At Lower Reynolds Numbers - صفحه:106-112

  tick  Investigation Of Fin Changes Effects On Aerodynamic Performance Of Airship - صفحه:1-10

  tick  Model Predictive Fault Tolerant Control Of Two-Tethered Satellite System - صفحه:128-142

  tick  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

  tick  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

  tick  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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