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journal of aerospace science and technology
سال:2011 - دوره:8 - شماره:1
A Novel Approach to Design of Truss-Beams for Natural Frequency
- صفحه:21-28
A Simple Explicit Guidance Scheme Based on Velocities-to-be-Gained
- صفحه:36-29
Determination of the best-fitting reference orbit for a LEO satellite using the Lagrange coefficients
- صفحه:37-44
Nonlinear Post-Buckling Analysis of Isotropic Plates Using Finite Strip Methods
- صفحه:11-19
Trim and Maneuverability Analysis Using a New Constrained PSO Approach of a UAV
- صفحه:45-56
Verification of a CFD solver in near ground effect for aerodynamic behavior of airfoil NACA 0015
- صفحه:1-10
Wave Propagation Approach to Fluid Filled Submerged Visco-Elastic Finite Cylindrical Shells
- صفحه:57-67
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