-Infinity Leveraging Boundary-Value Problem and Application in Spacecraft Trajectory Design
Vertical-Axis Wind Turbine Steady and Unsteady Aerodynamics for Curved Deforming Blades
Velocity-Potential Boundary-Field Integral Formulation for Sound Scattered by Moving Bodies
Unmanned Aerial Vehicles Evolutional Flight Route Planner Using the Potential Field Approach
Synthesis of Ballistic Capture Corridors at Mars via Polynomial Chaos Expansion
Supersonic Flutter Analysis Based on a Local Piston Theory
Study of Flexible Aircraft Body Freedom Flutter with Robustness Tools
Stall Cell Prediction Using a Lifting-Surface Model
Spanwise Variations in Aerodynamic Damping of an Oscillating Annular Compressor Cascade
Solar Polar Imaging Mission Design Leveraging Venus Flybys
Simultaneous Motion Replanning and Gravity Model Refinement near Small Solar System Bodies
Sensor Selection and Optimization for Health Assessment of Aerospace Systems
Satellite Relative Motion Modeling and Estimation via Nodal Elements
Reply by the Author(s) to K. Chen, L. Yue, and X. Chang
Receptance-Based Active Aeroelastic Control with Embedded Control Surfaces Having Actuator Dynamics
Reachable Set of Low-Delta- Trajectories Following a Gravity-Assist Flyby
Reachable Domain of Spacecraft After a Gravity-Assist Flyby
Physics of Vibrating Turbine Airfoils at Low Reduced Frequency
Performance Enhancement of Global Optimization-Based Gas Turbine Fault Diagnosis Systems