Experimental studies of airliner aerodynamic characteristics at overcritical angles of attack
Neural network modeling of unsteady aerodynamic characteristics at high angles of attack
The influence of Chine nose shapes on a slender body flight vehicle at high angles of attack
Research on light aircraft spinning properties
Static Force Measurement Technology Wind Tunnel Test
Reorientation of a Spinning Spacecraft with a Fixed Nonimpulsive Torque Thruster
Performance of a hydrofoil operating close to a free surface over a range of angles of attack
Dynamic Modeling from Flight Data with Unknown Time Skews
Control of a Minimally Actuated Biomimetic Vehicle Using Quarter-Cycle Wingbeat Modulation