Aerodynamic Performance Estimation of Camber Morphing Airfoils for Small Unmanned Aerial Vehicle

Abstract

This paper proposes a methodology to harvest the benefits of camber morphing airfoils for small unmanned aerial vehicle (SUAV) applications. Camber morphing using discrete elements was used to morph the base airfoil, which was split into two, three, and four elements, respectively, to achieve new configurations, into the target one. . In total, thirty morphed airfoil configurations were generated and tested for aerodynamic efficiency at the Reynolds numbers of 2.5 × 105 and 4.8 × 105, corresponding to loiter and cruise Reynolds numbers of a typical SUAV. The target airfoil performance could be closely achieved by combinations of 5 to 8 morphed configurations, the best of which were selected from a pool of thirty morphed airfoil configurations for the typical design specifications of SUAV. Interestingly, some morphed airfoil configurations show a reduction in drag coefficient of 1.21 to 15.17% compared to the target airfoil over a range of flight altitudes for cruise and loiter phases. Inspired by the drag reductions observed, a case study is presented for resizing a SUAV accounting for the mass addition due to the morphing system retaining the benefits of drag reduction.

An Experimental and Simulation Study of the Active Camber Morphing Concept on Airfoils Using Bio-Inspired Structures

“…The predominant focus of previous research on morphing technology’s computational performance has been on aerodynamic studies of specific morphing configurations and their associated processes [ 31 , 32 ], as well as on the deformation and power consumption of morphing designs. The primary objective of this study is to quantify the benefits of morphing wings in terms of drag reduction by comparing various camber morphing rates with different configurations of conventional wings created for different flap deflection angles.…”

“…Morphing the geometry of an aircraft’s wing during flight allows for enhanced flight performance across a broader range of flight conditions. Among various methods, camber morphing has emerged as a highly effective and efficient approach for achieving optimal efficiency throughout the entirety of a flight mission [ 31 ]. The conventional control systems such as flaps and ailerons, while capable of altering airflow, introduce discontinuities on the wing surface, leading to aerodynamic losses.…”