شماره 2 تاریخ انتشار 2017-12-01

• Fatigue Life Assessment of Composite Airplane Wing Subjected to Variable Mechanical and Thermal Loads
• A Parametric Study for Vibration Analysis of Composite Cylindrical Shell Resting under Elastic Foundation: Analytical and Numerical Methods
• Adaptive Quaternion Attitude Control of Aerodynamic Flight Control Vehicles
• Buckling and Post-buckling Analysis of FG-CNTRC Beams: An Exact Closed Form Solution
• Optimization of Composite Stiffened Cylindrical Shell using PSO Algorithm
• Optimization of Sound Transmission Loss of a Composite Rectangular Plate with Infinite Baffle