Contribution of spanwise and cross-span vortices to the lift generation of low-aspect-ratio wings: Insights from force partitioning

TL;DR

This paper investigates how different vortex structures around low-aspect-ratio wings contribute to lift, using a force partitioning method to distinguish the effects of spanwise and cross-span vortices.

Contribution

It introduces a force partitioning approach to quantify the lift contributions of specific vortex structures in low Reynolds number flows over low aspect-ratio wings.

Findings

Spanwise vortices contribute less to lift than cross-span vortices.

Near-wake spanwise vorticity can produce negative lift.

Force partitioning effectively reveals flow physics of vortex-dominated flows.

Abstract

This study reports on the vortex-induced lift production mechanisms in low Reynolds number flows over low aspect-ratio rectangular wings. We use a rigorous force partitioning method which allows for the estimation of the pressure-induced aerodynamic loads due to distinct flow features or vortex structures in the flow around the wing. The specific focus of this work is on distinguishing the effect of spanwise and cross-span oriented vortex structures on pressure-induced lift production. We quantify the lift induced on the wing by these different vortices, and also estimate their influence within different regions of the flow-field around the wing and in the wake. By varying the aspect-ratio and angle-of-attack of the wing, we show that for most cases, the spanwise oriented vorticity contributes less to the total lift than cross-span oriented vortices. Furthermore, the spanwise vorticity in the near wake is capable of producing net negative lift on the wing and this is explained by separating and quantifying the influence of vortex cores and regions of strain in the wake. The results demonstrate the utility of the force partitioning method for dissecting the flow physics of vortex dominated flows.