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Journal Of Aerospace Science And Technology
  
سال:2020 - دوره:13 - شماره:2
  
 
A Simulation Algorithm For Staged Combustion Cycle Liquid Propellant Rocket Engines
- صفحه:85-91
  
 
Analysis Of Torsional Hysteresis Behavior Of Shaft
- صفحه:67-72
  
 
Conceptual Design Of Aeroderivative Industrial Gas Turbines
- صفحه:37-46
  
 
Design Of Deterministic Self-Tuning Regulators For The Pitch Angle Of An Aircraft
- صفحه:61-66
  
 
Experimental Study Of The Spray Pattern Of A Non-Newtonian Gelled Fluid Using Two Impinging Jets
- صفحه:125-134
  
 
Investigating Cooperative And Non-Cooperative Interference Elimination Between Aircraft Using Game Theory
- صفحه:103-113
  
 
Investigating The Effects Of Noise And Parameter Changing On Modeling Of Jet Transport Aircraft
- صفحه:47-52
  
 
Multi-Scale Modeling For Thermal Conductivity Analysis Of Epoxy Nanocomposite - Cnt
- صفحه:1-6
  
 
Numerical And Experimental Analysis Of Ballistic Behavior Of Ceramic-Reinforced Aluminum Matrix Composites Plates
- صفحه:7-26
  
 
Restricted Three-Body Problem Considering Perturbations Of Oblate Primaries
- صفحه:27-35
  
 
The Strategy Of Using Porous Material In Liquid Fuel Space Propulsion Injectors
- صفحه:73-84
  
 
Two-Phase Cfd Modeling Of Three- Dimensional Supercavitating Flows
- صفحه:53-60
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