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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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