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The Use of Active Flow Control on Combined Tilt Rotor & Tilt Wing Airplanes
This technology is a method to eliminate moving control surfaces on the wing, prop, tail and other surfaces of a tilt wing airplane. It accomplishes this by utilizing active flow control measures. The end result is a combination of tilted wing with active flow controls designed to reduce the power demand of the tilt rotor wing aircraft. Reduced power...
Published: 8/28/2024
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Inventor(s): Israel Wygnanski, Elisa Phillips, Garrett Kay
Keywords(s):
Category(s): Technology Classifications > Engineering & Physical Sciences > Aerospace Engineering
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