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The Propulsive Wing is a new patented aerodynamic platform that integrates an
embedded, distributed cross-flow fan propulsion system within a thick wing.
Early research was conducted at Syracuse University under funding from NASA
Glenn Research Center. Propulsive Wing, LLC was formed in 2006 to facilitate
commercialization of this technology as a new unmanned aircraft to serve
commercial and military markets, with particular emphasis on applications
requiring large internal volume, heavy load-carrying capability, and short
takeoff and landing.
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The Propulsive Wing PW-4 prototype is currently undergoing flight-testing and will soon be available for demonstrations.
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| CFD simulation of the Propulsive Wing UAV at high angle of attack. Due to the unique patented design, the wing is capable of operating stall-free at extreme angle of attack, producing exceptionally high lift. For the same wingspan, the lifting capability of this platform is 2-3 times and the internal payload volume is up to 10 times conventional UAV configurations. |
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