Characterising the performance benefits of a 1/7th scale morphing rotor blade

Abstract

Rotary-wing aircrafts serve as indispensable components in the advancement of aviation, valued for their ability to operate in diverse and challenging environments without the need for conventional runways. This versatility makes them ideal for applications such as environmental conservation, precision agriculture, emergency medical support, and rapid-response operations in rugged terrains. However, although highly manoeuvrable, rotary-wing platforms generally have lower aerodynamic efficiency than fixed-wing aircraft. This study aims to improve aerodynamic performance by examining a 1/7th-scale rotor blade model equipped with a NACA0012 airfoil using CROTOR software. The analysis focuses on optimal spanwise locations for separating morphing and fixed blade sections at 85%, 90%, and 95% of the blade radius with up to +20 degrees of twist incorporated into the design. Key performance metrics assessed in this investigation include lift coefficient (CL), drag coefficient (CD), lift-to-drag ratio (CL/CD), Mach number, power, thrust coefficient, and Figure of Merit (FOM). Results indicate that the 0.90 r/R position is optimal for dividing the morphing and fixed sections, achieving a significant improvement of over 7% in both lift-to-drag ratio and FOM. These findings underscore the substantial impact on the overall performance of the rotor system and rotational aerodynamics that geometric modifications through the inclusion of a morphing capability can ultimately realise.