The flying wing configuration represents an advanced tailless aerodynamic design. However, due to its lack of lateral-directional stability, it tends to experience wing rock at high angles of attack, posing challenges for attitude control. This manuscript proposes a synergistic control strategy based on the mechanism of leading-edge vortex (LEV) control and recirculation zone (RZ) control, achieved through inward-directed jets at the leading edge. Wind tunnel experiments demonstrate that this strategy enables a continuously variable regulation of the roll attitude between 27° to the right and 27° to the left, exhibiting control capabilities comparable to ailerons. Furthermore, quantitative analysis of the flow field and pressure indicates interactions between the jet and the flow structures cause asymmetrical effects on the pressures on both wing sides, thus generating a positive rolling moment. Specifically, the jet-induced vortex (JIV) generated by LEV control lifts the LEV, distancing it from the wing surface, thereby reducing the vortex lift. Additionally, JIV enhances the normal oscillation of the LEV, leading to LEV breakdown and a decrease in the induced negative pressure peak. RZ control injects momentum into the RZ and reduces its size, thereby suppressing flow separation and enhancing the negative pressure on that side of the wing. The above investigation establishes a crucial foundation for substituting conventional mechanical control surfaces and achieving virtual aerodynamic surface control.
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