Nonlinear Instabilities in a Single-axis Vibratory Gyroscope AIAA Paper 2007-2210 CD-ROM Number 8
Attenuation of Self-Excited Roll Oscillations of Low-Aspect-Ratio Wings by Using Acoustic Forcing
Attenuation of Self-Excited Roll Oscillations of Low-Aspect-Ratio Wings by Using Acoustic Forcing
Impact Analysis of the Leap Second to the Computer System in Beijing Aerospace Control Center
Modeling post-shock emergency transfers with the participation of connected-and-autonomous vehicles
AN INVESTIGATION ON THE IMPROVEMENT FOR TANDEM WING PITCHING MOMENT CHARACTERISTICS
The Analysis of 16MnR Steel Compact Tensile Fatigue Fracture after High Temperature
Effective Application of CAE Guidance for Hemmed Closures Throughout the Vehicle Development Process
Effective Application of CAE Guidance for Hemmed Closures Throughout the Vehicle Development Process