Additional Wind Tunnel Testing of a Lift-Augmented Quadcopter

Staub, Franco M.; Premeaux, Emery; Tsukada, Dai; Inoue, Shota; Raabe, Christopher T.; Tsuchiya, Takeshi

doi:10.2514/6.2022-2479

Cited by 1 publication

(2 citation statements)

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“…The authors in [22][23][24] present the design and aerodynamic testing of a quadcopter with short lifting wings attached at a fixed angle to the frame. The authors develop a model in [22] by balancing aerodynamic forces on the vehicle and assuming power consumption varies as a cubic function airspeed.…”

Section: B Suas Wind Tunnel Testingmentioning

confidence: 99%

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Wind Tunnel Testing and Aerodynamic Characterization of a QuadPlane Uncrewed Aircraft System

Mathur¹,

Atkins²

2023

Preprint

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Electric Vertical Takeoff and Landing (eVTOL) vehicles will open new opportunities in aviation. This paper describes the design and wind tunnel analysis of an eVTOL uncrewed aircraft system (UAS) prototype with a traditional aircraft wing, tail, and puller motor along with four vertical thrust pusher motors. Vehicle design and construction are summarized. Dynamic thrust from propulsion modules is experimentally determined at different airspeeds over a large sweep of propeller angles of attack. Wind tunnel tests with the vehicle prototype cover a suite of hover, transition and cruise flight conditions. Net aerodynamic forces and moments are distinctly computed and compared for plane, quadrotor and hybrid flight modes. Coefficient-based models are developed. Polynomial curve fits accurately capture observed data over all test configurations. To our knowledge, the presented wind tunnel experimental analysis for a multi-mode eVTOL platform is novel. Increased drag and reduced dynamic thrust likely due to flow interactions will be important to address in future designs.

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Section: B Suas Wind Tunnel Testingmentioning

confidence: 99%

“…It was shown that endurance can be improved by up to 33% with lifting wings. The same platform was augmented with a blended wing-body design and a trailing edge flap in [24] and tested inside a wind tunnel with the wing mounted at 30°. Lift and Drag coefficients for the vehicle with different flap deflections were plotted.…”

Section: B Suas Wind Tunnel Testingmentioning

confidence: 99%

Wind Tunnel Testing and Aerodynamic Characterization of a QuadPlane Uncrewed Aircraft System

Mathur¹,

Atkins²

2023

Preprint

View full text Add to dashboard Cite

show abstract

Additional Wind Tunnel Testing of a Lift-Augmented Quadcopter

Cited by 1 publication

References 2 publications

Wind Tunnel Testing and Aerodynamic Characterization of a QuadPlane Uncrewed Aircraft System

Wind Tunnel Testing and Aerodynamic Characterization of a QuadPlane Uncrewed Aircraft System

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