Design and Development of Sikorsky's Rotor Blown Wing Demonstrator

Marc Regan, Vera Klimchenko, Cal Sargent, Brian Wallace, Antonio Rivera, Jordan Kaye, Jason Satira, Patrick Bowles, Dustin Coleman


Presented at the Vertical Flight Society 81th Annual Forum & Technology Display
Test and Evaluation Technical Session
19 pages

https://doi.org/10.4050/F-0081-2025-200

 

Abstract:
The Rotor Blown Wing (RBW) is a tailsitter Vertical Takeoff and Landing (VTOL) Unmanned Aerial System (UAS) configuration that leverages cutting-edge autonomous flight controls through Sikorsky's MATRIX™ technology to create a highly capable, efficient, and scalable technology platform. By combining the benefits of fixed- and rotary-wing aircraft, the RBW configuration eliminates the need for traditional UAS launch and recovery infrastructure. This paper describes the RBW-5 prototype, a 100-pound, dual 5-foot diameter proprotor demonstrator, and discusses the comprehensive evaluation of its design and operability through a combination of flight tests, wind tunnel experiments, and computational fluid dynamics (CFD) simulations. The results demonstrate the maturity of the UAS and highlights key accomplishments of the RBW-5 program, including successful autonomous takeoff and landing and transitions between hover and forward flight, the extraction of critical "blown-physics" underlying RBW aerodynamics, and the validation of CFD models against unpowered and powered wind tunnel data.

 

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