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Journal Of Aerospace Science And Technology
  
سال:2006 - دوره:3 - شماره:1
  
 
Application Of A Simulation Algorithm For Dynamic Analysis Of A Liquid Propellant Engine
- صفحه:23-31
  
 
Experimental Study Of Vortex Shapes Behind A Wing Equipped With Different Winglets
- صفحه:1-16
  
 
Les Numerical Study Of Reynolds Number Effects On Flow Over A Wall-Mounted Cube In A Channel
- صفحه:51-60
  
 
Nonlinear Optimal Control Techniques Applied To A Launch Vehicle Autopilot
- صفحه:43-50
  
 
Numerical Simulation Of Flow Past Oscillating Airfoil Using Oscillation Of Flow Boundary Condition
- صفحه:17-22
  
 
Selection Of Favorite Reusable Launch Vehicle Concepts By Using The Method Of Pairwise Comparison
- صفحه:31-42
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