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journal of aerospace science and technology
سال:2005 - دوره:2 - شماره:4
Effect of Amplitude and Mean Angle of Attack on the Unsteady Surface Pressure of a Pitching Airfoil
- صفحه:9-26
Experimental Studies of Inverted-Profile Coaxial Jet Flows
- صفحه:1-8
Orr Sommerfeld Solver Using Mapped Finite Difference Scheme for Plane Wake Flow
- صفحه:55-63
Robust Optimal Control of Flexible Spacecraft During Slewing Maneuvers
- صفحه:37-43
Time Optimal Closed-Loop Fuzzy-Control St rategy for Nonlinear Lunar Lander Mission
- صفحه:27-36
Transonic and Supersonic Overtaking of a Projectile Preceding a Shock Wave
- صفحه:45-53
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