Abstract: Means are described for controlling the asymmetry of the leeside vortices developing over a pointed object placed at an angle of attack in a flowing fluid. Unlike prior art, the stagnation point controller biases the vortices at their point of origin. Resulting devices enable rapid and precise control of vortex asymmetry. The amplitude and rate of such motion is used to control the amplitude and rate of the asymmetry. Complex types of variations in asymmetry are demonstrated. The stagnation point controller is used in inventing means of controlling the yawing and rolling moments of aircraft and other solid objects at high angle of attack in fluid flow.

Abstract: A wind driven aerodynamic manipulator is provided for imparting motion to an aerodynamic model located in a wind tunnel. The manipulator comprises a support for supporting an aerodynamic body within a wind tunnel; a first aerodynamic surface affixed to the support in such a manner as to allow motion to be imparted to the aerodynamic body by an interaction between the first aerodynamic surface and a fluid flow within the wind tunnel; and a first controller for orienting the first aerodynamic surface with respect to the fluid flow. Additionally, a multi-dimensional manipulator is also disclosed.