Injector slots on the airfoil suction side boost laminar airflow and lift, enabling Super-STOL flight with less system complexity.
Injector slots direct air from the leading edge across the suction side to sustain laminar flow, augment lift, and avoid external air intakes.
Rotor downwash can cause flow separation near wings; placing rotors behind and below the airfoil uses suction to increase lift and counter drag.
Actuators induce traveling waves along exposed surfaces to damp supersonic shocks, reduce turbulence, and limit material fatigue.