An Assessment of a Regional Turboprop Featuring Wingtip-Mounted Propellers
Design Integration Coupling Propeller-Wing Aerodynamics and Structural Wing Weight
Quinty van der Leer (TU Delft - Aerospace Engineering)
M.F.M. Hoogreef – Mentor (TU Delft - Flight Performance and Propulsion)
B.F. Lopes Dos Santos – Graduation committee member (TU Delft - Air Transport & Operations)
L.L.M. Veldhuis – Graduation committee member (TU Delft - Flight Performance and Propulsion)
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Abstract
The current focus in the aviation industry for more sustainable designs, could mean the revive of propeller propulsion, due to their relative high propulsion efficiency compared to jets. In addition, the application of wingtip-mounted propellers installed in tractor configuration can be used as tip-vortex attenuating devices, reducing the wing induced drag. The wingtip-mounted propeller configuration is believed to offer a significant aircraft performance benefit from an aerodynamic perspective. So far, studies on wingtip-mounted propellers mainly concentrated on the aerodynamic interaction effects, disregarding the integration with the airframe and wing-structural mass. This thesis presents a methodology to integrate aerodynamic, aero-propulsive, and aero-structural effects of tip-mounted propellers in the context of a typical turboprop featuring hybrid-electric propulsion. The developed methodology is used to assess the effect of wingtip-mounted propellers on both wing and aircraft level, providing new insights in the potential of the configuration.