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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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