Wingtip-mounted propellers: Aerodynamic analysis of interaction effects and comparison with conventional layout

T Sinnige, N van Arnhem, TCA Stokkermans… - Journal of Aircraft, 2019 - arc.aiaa.org
Wingtip-mounted propellers installed in a tractor configuration can decrease the wing
induced drag by attenuating the wingtip vortex by the propeller slipstream. This paper …

Validation and comparison of RANS propeller modeling methods for tip-mounted applications

TCA Stokkermans, N Van Arnhem, T Sinnige… - AIAA Journal, 2019 - arc.aiaa.org
The potentially favorable interaction of a propeller slipstream with a wingtip is a complex
problem, because of the importance of vortex interaction and viscous effects. This paper …

Stable vortex particle method formulation for meshless large-eddy simulation

EJ Alvarez, A Ning - AIAA Journal, 2024 - arc.aiaa.org
A novel formulation of the vortex particle method (VPM) is developed for large-eddy
simulation (LES) in a meshless scheme that is numerically stable. A new set of VPM …

Rans-based aerodynamic shape optimization of a wing considering propeller–wing interaction

SS Chauhan, JRRA Martins - Journal of Aircraft, 2021 - arc.aiaa.org
The recent growth of interest in hybrid-electric and fully electric aircraft has led to a renewed
focus on the design and optimization of propeller aircraft. Considering propeller–wing …

FLOWUnsteady: an interactional aerodynamics solver for multirotor aircraft and wind energy

EJ Alvarez, J Mehr, A Ning - AIAA Aviation 2022 Forum, 2022 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2022-3218. vid The ability to accurately
and rapidly assess unsteady interactional aerodynamics is a shortcoming and bottleneck in …

Impingement of a propeller-slipstream on a leading edge with a flow-permeable insert: A computational aeroacoustic study

F Avallone, D Casalino… - International Journal of …, 2018 - journals.sagepub.com
This manuscript describes an aeroacoustic computational study on the impingement of a
tractor-propeller slipstream on the leading edge of a pylon. Both the flow and acoustic fields …

RANS-Based Aerodynamic Shape Optimization of a Wing with a Propeller in Front of the Wingtip

SS Chauhan, JRRA Martins - Aerospace, 2024 - mdpi.com
Accounting for propeller–wing interaction allows for the design of more efficient propeller
aircraft through strategic propulsion integration. In this paper, the cruise drag of a wing with a …

Alleviation of propeller-slipstream-induced unsteady pylon loading by a flow-permeable leading edge

T Sinnige, BD Corte, R De Vries, F Avallone… - Journal of Aircraft, 2019 - arc.aiaa.org
The impingement of a propeller slipstream on a downstream surface causes unsteady
loading, which may lead to vibrations responsible for structure-borne noise. A low-speed …

Experimental investigation of over-the-wing propeller–boundary-layer interaction

R de Vries, N van Arnhem, F Avallone, D Ragni, R Vos… - AIAA Journal, 2021 - arc.aiaa.org
This experimental study focuses on the aerodynamic interaction between an over-the-wing
(OTW) propeller and a wing boundary layer. An OTW propeller is positioned above the …

Aerodynamic interaction effects of tip-mounted propellers installed on the horizontal tailplane

N Arnhem, T Sinnige, TC Stokkermans… - 2018 AIAA Aerospace …, 2018 - arc.aiaa.org
Driven by the desire for high subsonic flight, the major focus of aircraft engine development
is on turbofan engines. However, the constant pursuit of higher propulsive efficiency …