Buckling Modes of Thin Circular Cylindrical Shells Under Fundamental Loads (TN)
Development and static strength proof of the aircraft wing structure manufactured by VaRTM
Protection Systems for Optical Access Networks (Invited Paper)
Integrated control of active rear wheel steering and direct yaw moment control
Multi-Objective Stacking Sequence Optimization of Composite Wing Structure Using FBBM AIAA Paper
Burst-mode Q-switching operation of a Nd:YAG rod laser [3889-23]