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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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