شماره 1 تاریخ انتشار 2634-04-21

• Implementation of "MSG-3" for Crack Growth Analysis of Aircraft SSI Components
• Rotor Sizing of Helicopters Using Statistical Approach
• Extracting Dynamics Matrix of Alignment Process for a Gimbaled Inertial Navigation System Using Heuristic Dynamic Programming Method
• Simulation of Pitching and Heaving Airfoil with Oscillation of Flow Boundary Condition
• A Three Stage Terminal Fuzzy Guidance Law for Reentry Vehicles
• Nonlinear Dynamic Modeling and Hysteresis Analysis of Aerospace Hydro - dynamical Control Valves