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journal of aerospace science and technology
  
سال:2022 - دوره:15 - شماره:1
  
 
Designing an Ultrasonic Wind Tunnel with a Steam Ejector System of Combined Cycle Power Plants
- صفحه:27-36
  
 
Designing the Nonlinear Guidance Law Adaptable to Initial Deviations for the Vertical Landing of the Booster
- صفحه:15-26
  
 
Development of Nonlinear Model and Implementation of Real-Time Flight Simulation of a Flexible Projectile in Simulink Environment for Initial Design and Stability Analysis
- صفحه:99-118
  
 
Development of Vision-Based Human Tracking for Drone’s Gimbal
- صفحه:61-70
  
 
Mixed Mode (I/II/III) Stress Intensity Factors in Gas Turbine Blade Considering 3D Semi-Elliptical Crack
- صفحه:1-13
  
 
Noise-Induced Miss Distance Analysis of First-Order Explicit Guidance Law
- صفحه:129-139
  
 
Numerical Calculation of Radiation Heating of the Hypersonic Nose in the Reentry Phase
- صفحه:49-60
  
 
Numerical study on enhancement of low speed axial compressor rotor performance under radial inlet distortion via DBD plasma actuators
- صفحه:117-128
  
 
Simulation of the Effect of Using a Finned Tube on the Thermal Efficiency of Shell and Tube Heat Exchangers
- صفحه:83-98
  
 
Sliding Mode Stabilization of Quad Tilt-wing UAV Considering Nonlinear Model of the Vehicle and Uncertainties
- صفحه:37-48
  
 
Static and Dynamic Analyses of Integral Pulse-Width Pulse-Frequency Modulator with Small Error-Reset Integrator Logical Circuit
- صفحه:73-82
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